阅读说明：本技术 通道校正的方法和装置 (Method and device for channel correction ) 是由 熊鑫 于 2019-03-22 设计创作，主要内容包括：本申请提供了一种通道校正的方法和装置。应用在多个RRU中的每两个RRU之间的收发通道校正,包括：第一RRU通过至少两个天线以第一发射功率和第一权值向量向第二RRU中的至少两个天线发送校正参考信号,第二RRU接收到的校正参考信号合并为第五校正参考信号；第一RRU通过至少两个天线接收第二RRU中的至少两个天线发送的校正参考信号,第一RRU接收到的校正参考信号合并为第六校正参考信号；第五校正参考信号和第六校正参考信号用于计算校正系数。本申请提供的技术方案可以避免RRU接收到的校正参考信号信噪比过低或功率过高导致无法实现RRU之间的收发通道校正,提高RRU之间的收发通道校正性能。(The application provides a method and a device for channel correction. The method for correcting the transceiving channel between every two RRUs in the plurality of RRUs comprises the following steps: the first RRU sends correction reference signals to at least two antennas in the second RRU through at least two antennas by using first transmission power and a first weight vector, and the correction reference signals received by the second RRU are combined into a fifth correction reference signal; the first RRU receives correction reference signals sent by at least two antennas in the second RRU through at least two antennas, and the correction reference signals received by the first RRU are combined into a sixth correction reference signal; the fifth correction reference signal and the sixth correction reference signal are used to calculate a correction coefficient. The technical scheme provided by the application can avoid that the receiving and transmitting channel correction between the RRUs cannot be realized due to the fact that the signal-to-noise ratio of the correction reference signal received by the RRUs is too low or the power is too high, and the receiving and transmitting channel correction performance between the RRUs is improved.)

1. A method for correcting a transceiving channel between a first Remote Radio Unit (RRU) and a second RRU is characterized in that the first RRU comprises a first antenna and a second antenna, the second RRU comprises a third antenna and a fourth antenna, and the method comprises the following steps:

the first RRU sends a first correction reference signal to the third antenna and the fourth antenna through the first antenna by using first transmission power and a first weight vector;

the first RRU sends a second correction reference signal to the third antenna and the fourth antenna through the second antenna by using the first transmission power and the first weight vector;

the first RRU receives a third correction reference signal which is sent by the second RRU through the third antenna by using second transmission power and a second weight vector through the first antenna and the second antenna;

the first RRU receives a fourth correction reference signal which is sent by the second RRU through the fourth antenna by using second transmission power and a second weight vector through the first antenna and the second antenna;

the first transmit power is a transmit power in a preset first transmit power set, and the first weight vector is a weight vector in a preset first weight vector set; the second transmitting power is the transmitting power in a preset second transmitting power set, and the second weight vector is the weight vector in a preset second weight vector set;

the corrected reference signal received at the third antenna and the corrected reference signal received at the fourth antenna are combined into a fifth corrected reference signal, and the corrected reference signal received at the first antenna and the corrected reference signal received at the second antenna are combined into a sixth corrected reference signal; the fifth correction reference signal and the sixth correction reference signal are used for calculating a correction coefficient of a transceiving channel between the first RRU and the second RRU.

2. The method of claim 1, wherein the fifth corrected reference signal is obtained by:

the fifth calibration reference signal is obtained by multiplying the calibration reference signal received at the third antenna by the weight corresponding to the third antenna in the second weight vector, and the calibration reference signal received at the fourth antenna, and the sum of the calibration reference signal obtained by multiplying the calibration reference signal received at the fourth antenna by the weight corresponding to the fourth antenna in the second weight vector.

3. The method according to claim 1 or 2, wherein the sixth corrected reference signal is obtained by:

the sixth calibration reference signal is obtained by multiplying the calibration reference signal received at the first antenna by the weight corresponding to the first antenna in the first weight vector, and the calibration reference signal received at the second antenna, and multiplying the correction reference signal obtained by multiplying the weight corresponding to the second antenna in the first weight vector.

4. The method according to any of claims 1-3, wherein the first calibration reference signal is a calibration reference signal obtained by multiplying a preset calibration reference signal by a weight corresponding to the first antenna in the first weight vector, and the second calibration reference signal is a calibration reference signal obtained by multiplying the preset calibration reference signal by a weight corresponding to the second antenna in the first weight vector.

5. The method of any of claims 1-4, wherein an optional set comprises at least one optional subset of sets, wherein the optional subset of sets comprises transmit power and weight vectors that can be used by the first RRU and transmit power and weight vectors that can be used by a second RRU, and wherein a first optional subset of the at least one optional subset of sets comprises the first transmit power, the first weight vector, the second transmit power, and the second weight vector.

6. The method of claim 5, wherein the first subset of selectable sets corresponds to a first received power, a second received power, a third received power, a fourth received power, a signal-to-noise ratio of the fifth calibration reference signal, and a signal-to-noise ratio of the sixth calibration reference signal, wherein the first received power, the second received power, the third received power, and the fourth received power satisfy a predetermined power threshold, and wherein the signal-to-noise ratio of the fifth calibration reference signal and the signal-to-noise ratio of the sixth calibration reference signal satisfy a predetermined signal-to-noise ratio threshold;

wherein the first received power is a power of a calibration reference signal received at the first antenna, the second received power is a power of a calibration reference signal received at the second antenna, the third received power is a power of a calibration reference signal received at the third antenna, and the fourth received power is a power of a calibration reference signal received at the fourth antenna.

7. The method of claim 6, wherein the SNR of the fifth calibration reference signal and the SNR of the sixth calibration reference signal that are smaller than the median are the SNR with the largest median of a plurality of SNRs, and wherein the SNRs are the SNRs with smaller median of two SNRs corresponding to the plurality of subsets of the selectable sets.

8. A first Remote Radio Unit (RRU) is used for correcting a receiving and sending channel between the RRU and a second RRU, and is characterized in that the first RRU comprises a first antenna and a second antenna, and the antenna sends a first correction reference signal to a third antenna and a fourth antenna by first transmission power and a first weight vector;

the transmitting unit is further configured to transmit, through the second antenna, a second correction reference signal to the third antenna and the fourth antenna at the first transmit power and the first weight vector;

a receiving unit, configured to receive, through the first antenna and the second antenna, third calibration reference signals that are respectively sent by the second RRU through the third antenna and the fourth antenna with a second transmit power and a second weight vector;

the receiving unit is further configured to receive, through the first antenna and the second antenna, a fourth calibration reference signal sent by the second RRU through the fourth antenna with a second transmit power and a second weight vector;

the first transmit power is a transmit power in a preset first transmit power set, the first weight vector is a weight vector in a preset first weight vector set, the second transmit power is a transmit power in a preset second transmit power set, and the second weight vector is a weight vector in a preset second weight vector set;

the corrected reference signal received at the third antenna and the corrected reference signal received at the fourth antenna are combined into a fifth corrected reference signal, and the corrected reference signal received at the first antenna and the corrected reference signal received at the second antenna are combined into a sixth corrected reference signal; the fifth correction reference signal and the sixth correction reference signal are used for calculating a correction coefficient of a transceiving channel between the first RRU and the second RRU.

9. The first RRU of claim 8, wherein the fifth calibration reference signal is obtained by:

the fifth calibration reference signal is obtained by multiplying the calibration reference signal received at the third antenna by the calibration reference signal obtained by multiplying the weight corresponding to the third antenna in the second weight vector and the calibration reference signal received at the fourth antenna, and multiplying the calibration reference signal obtained by multiplying the weight corresponding to the fourth antenna in the second weight vector.

10. The first RRU according to claim 8 or 9, wherein the sixth corrected reference signal is obtained by:

the sixth calibration reference signal is obtained by multiplying the calibration reference signal received at the first antenna by the weight corresponding to the first antenna in the first weight vector, and the calibration reference signal received at the second antenna, and multiplying the correction reference signal obtained by multiplying the weight corresponding to the second antenna in the first weight vector.

11. The first RRU of any of claims 8-10, wherein the first corrected reference signal is

Presetting a correction reference signal which is obtained by multiplying the correction reference signal by a weight corresponding to the first antenna in the first weight vector;

the second calibration reference signal is a calibration reference signal obtained by multiplying the preset calibration reference signal by a weight corresponding to the second antenna in the first weight vector.

12. The first RRU of any of claims 8-11, wherein an optional set comprises at least one optional subset of sets, wherein the optional subset of sets comprises transmit power and weight vectors that can be used by the first RRU and transmit power and weight vectors that can be used by a second RRU, and wherein a first optional subset of the at least one optional subset of sets comprises the first transmit power, the first weight vector, the second transmit power, and the second weight vector.

13. The first RRU of claim 12, wherein the first subset of selectable sets corresponds to a first receive power, a second receive power, a third receive power, a fourth receive power, a signal-to-noise ratio of the fifth calibration reference signal, and a signal-to-noise ratio of the sixth calibration reference signal, wherein the first receive power, the second receive power, the third receive power, and the fourth receive power satisfy a predetermined power threshold, and wherein the signal-to-noise ratio of the fifth calibration reference signal and the signal-to-noise ratio of the sixth calibration reference signal satisfy a predetermined signal-to-noise ratio threshold;

wherein the first received power is a power of a calibration reference signal received at the first antenna, the second received power is a power of a calibration reference signal received at the second antenna, the third received power is a power of a calibration reference signal received at the third antenna, and the fourth received power is a power of a calibration reference signal received at the fourth antenna.

14. The first RRU of claim 13, wherein the snr of the fifth and sixth calibration reference signals that is the smallest of the snrs is the largest of a plurality of snrs, wherein the plurality of snrs are the smallest of the snrs corresponding to the at least one subset of the selectable sets.

15. An apparatus for channel correction, comprising:

a memory for storing a computer program;

a transceiver for performing transceiving steps in the method of channel correction of any of claims 1-7;

a processor for invoking and running the computer program from the memory, causing the channel correction device to perform the method of channel correction of any of claims 1-7.

16. A computer program product, comprising:

computer program which, when executed, causes a computer to carry out the method of channel correction of any one of claims 1-7.

Technical Field

The present application relates to the field of communications, and more particularly, to a method and apparatus for channel correction.

Background

With the continuous development of communication technology, in order to improve the data transmission rate, a coordinated multi-point (CoMP) technology is introduced into a communication system. The CoMP technology is applied in a communication system on the premise that uplink Channel State Information (CSI) and downlink CSI satisfy reciprocity, where the CSI includes a null interface information portion and a Remote Radio Unit (RRU) information portion. According to the physical characteristics of the channel, if the air interface information part in the CSI meets the reciprocity requirement, it is mainly considered whether the RRU information part in the CSI meets the reciprocity requirement. Specifically, each RRU corresponds to a group of antenna arrays, and the RRUs have transceiver channels in the same number as the antennas in the antenna arrays, for example, if an antenna array of a certain RRU includes two antennas, two transceiver channels are provided in the corresponding RRU, and each transceiver channel includes one transceiver channel and one receiver channel. The RRU information part in the CSI can be divided into a channel information part in the RRU and a channel information part between the RRUs, and because the response of an analog device in the channel has temperature change and time change characteristics, the RRU information part between each antenna may not meet the uplink and downlink reciprocity, and the uplink and downlink reciprocity of the RRU information part between each antenna needs to be corrected online. Wherein, the uplink and downlink reciprocity correction of the RRU information part between the antennas comprises the following steps: and correcting reciprocity of the channel information part between the RRU and the channel information part in the RRU.

Firstly, in order to ensure reciprocity of channel information portions in RRUs, channel responses of transceiver channels in the RRUs need to be corrected, so that the ratio of the channel response of a transmitter channel to the channel response of a receiver channel of each transceiver channel in the RRUs is the same.

Further, in order to ensure that all antennas between the RRUs satisfy reciprocity, a method for correcting a channel information part between multiple RRUs is proposed in an existing communication system, and hereinafter, the channel information part between the RRUs is referred to as correction of a receiving and transmitting channel between the RRUs. After the receiving and sending channels between the RRUs are corrected, reciprocity is satisfied on all antennas in the communication system adopting the CoMP technology.

However, in the existing method for correcting the transceiving channel between the RRUs, when the signal-to-noise ratio of the correction reference signal received by the RRUs is too low or the power is too high, the transceiving channel between the RRUs cannot be corrected. Therefore, how to avoid that the calibration reference signal received by the RRUs has too low signal-to-noise ratio or too high power, which results in that the calibration of the transceiving channel between the RRUs cannot be realized, and improve the calibration performance of the transceiving channel between the RRUs becomes a problem to be solved urgently.

Disclosure of Invention

The application provides a method and a device for channel correction, wherein a sending end RRU between every two RRUs in a plurality of RRUs sends correction reference signals through at least two antennas by at least two antennas in a power and weight vector receiving end RRU, specifically, the correction reference signals respectively received by at least two antennas in the receiving end RRU are combined into a path of correction reference signals, a correction coefficient for correcting a receiving and sending channel between the two RRUs is calculated based on the correction reference signals received and combined by the two RRUs (any one RRU in every two RRUs can be used as the sending end RRU once and as the receiving end RRU once, and then two receiving end RRUs can be used), the problem that the receiving and sending channel correction between the two RRUs cannot be corrected due to the fact that the signal-to-noise ratio of the correction reference signals received by the receiving end RRUs is too low or the power is too high.

In a first aspect, a method for correcting a transceiving channel between a first remote radio unit RRU and a second RRU is provided, where the first RRU includes a first antenna and a second antenna, and the second RRU includes a third antenna and a fourth antenna, and the method includes: a first RRU sends a first correction reference signal to a third antenna and a fourth antenna through a first antenna and a second antenna by using first transmission power and a first weight vector, the first RRU sends a second correction reference signal to the third antenna and the fourth antenna by using the first transmission power and the first weight vector through the second antenna, and the first RRU receives a third correction reference signal sent by the second RRU through the third antenna by using second transmission power and a second weight vector through the first antenna and the second antenna; the first RRU receives a fourth correction reference signal which is sent by the second RRU through the fourth antenna by using second transmission power and a second weight vector through the first antenna and the second antenna; wherein the first transmit power is a transmit power in a preset first transmit power set, the first weight vector is a weight vector in a preset first weight vector set, the second transmit power is a transmit power in a preset second transmit power set, the second weight vector is a weight vector in a preset second weight vector set, the calibration reference signal received at the third antenna and the calibration reference signal received at the fourth antenna are combined into a fifth calibration reference signal, and the calibration reference signal received at the first antenna and the calibration reference signal received at the second antenna are combined into a sixth calibration reference signal; the fifth correction reference signal and the sixth correction reference signal are used for calculating a correction coefficient of a transceiving channel between the first RRU and the second RRU.

According to the channel correction method provided by the embodiment of the application, a sending end RRU in two RRUs selects proper power and weight vectors from a known transmitting power set and a weight vector set, and sends correction reference signals to at least two antennas in a receiving end RRU through at least two antennas in the sending end. Specifically, after at least two antennas in the receiving end RRU receive the calibration reference signal, a path of calibration reference signal can be obtained by combining the calibration reference signals. And finally, calculating a correction coefficient for correcting a receiving and transmitting channel between the two RRUs according to the correction reference signal received by the receiving end RRU. Because the sending end RRU sends the correction reference signal through at least two antennas with specific power and weight, the receiving end RRU can be ensured to avoid that the receiving end RRU cannot correct the receiving and sending channel between the two RRUs due to too low signal-to-noise ratio or too high power of the received correction reference signal when receiving the correction reference signal, thereby improving the correction performance of the receiving and sending channel between the RRUs.

It should be understood that in this embodiment of the present application, it is not limited that one communication system includes only the first RRU and the second RRU, and when the communication system includes multiple RRUs, the above scheme may be adopted for calculating the channel correction coefficient between every two RRUs, and details are not described in this application.

It should also be understood that each RRU is not limited to include only two antennas in the present application, and each RRU may include multiple antennas in the present application, where at least two antennas may be selected from the multiple antennas in the RRU at the transmitting end to transmit the calibration reference signal in the above process of calculating the third calibration reference signal and the fourth calibration reference signal.

It should also be understood that the subject application is not limited to the implementation of calculating the correction coefficients of the transceiving channel between the first RRU and the second RRU based on the third correction reference signal and the fourth correction reference signal. For example, the first RRU may perform the correction, and the second RRU may notify the first RRU of the calculated fourth correction reference signal value; or, the second RRU may perform the correction, and the first RRU may notify the second RRU of the calculated fourth correction reference signal value; if the correction is performed by the BBU connected to the first RRU, the second RRU may notify the first RRU of the calculated value of the fourth correction reference signal, and the first RRU acquires that the values of the third correction reference signal and the fourth correction reference signal are equal to the BBU connected to the first RRU or acquires the values of the third correction reference signal and the fourth correction reference signal; or the first RRU may be executed by a BBU connected to the second RRU, the first RRU may notify the second RRU of the calculated value of the fourth calibration reference signal, and the second RRU acquires values of the third calibration reference signal and the fourth calibration reference signal that are equal to the BBU connected to the second RRU or values of the third calibration reference signal and the fourth calibration reference signal; or the second RRU may notify the management device of the calculated fourth calibration reference signal value, and the first RRU may notify the management device of the calculated third calibration reference signal value.

Specifically, the preset first transmit power set and the preset first weight vector set are known sets of the first RRU, and the preset second transmit power set and the preset second weight vector set are known sets of the second RRU. It can be understood as a pre-configured set for the developer. In the present application, the size and number of the parameters included in the preset set (which may be referred to as a set, where the number of the parameters included in the preset set should be not less than two) are not limited, and may be configured by the developer according to a priori results, or configured by the developer according to experience.

Specifically, how to determine the first transmit power, the first weight vector, the second transmit power, and the second weight vector is not limited in the above process, because appropriate values may be selected from the preset first transmit power set, the preset first weight vector set, the preset second transmit power set, and the preset second weight vector set according to experience, or selected through calculation. How to select the first transmit power, the first weight vector, the second transmit power, and the second weight vector in a calculation manner will be described below, and details thereof will not be repeated here.

With reference to the first aspect, in certain implementations of the first aspect, the fifth correction reference signal may be obtained by: the sum of the corrected reference signal received at the third antenna multiplied by the weight corresponding to the third antenna in the second weight vector and the corrected reference signal received at the fourth antenna multiplied by the weight corresponding to the fourth antenna in the second weight vector is the fifth corrected reference signal.

With reference to the first aspect, in certain implementations of the first aspect, the sixth correction reference signal may be obtained by: the sum of the corrected reference signal received at the first antenna multiplied by the weight corresponding to the first antenna in the first weight vector, the corrected reference signal received at the second antenna multiplied by the weight corresponding to the second antenna in the first weight vector is the sixth corrected reference signal.

According to the channel correction method provided by the embodiment of the application, after at least two antennas in a receiving end RRU (a first RRU can be the receiving end RRU, and a second RRU can also be the receiving end RRU) receive a correction reference signal, a path of correction reference signal is obtained by combining the weight vectors of the correction reference signal sent by the receiving end RRU, and how to combine the correction reference signals received by multiple antennas can be determined, so that the combining accuracy is improved.

With reference to the first aspect, in some implementations of the first aspect, the first calibration reference signal is a calibration reference signal obtained by multiplying a preset calibration reference signal by a weight corresponding to the first antenna in the first weight vector; the second calibration reference signal is a calibration reference signal obtained by multiplying a preset calibration reference signal by a weight corresponding to the second antenna in the first weight vector.

According to the channel correction method provided by the embodiment of the application, when the sending end RRU sends the correction reference signal through at least two antennas, the sending end RRU sends the correction reference signal according to the weight corresponding to each antenna included in the determined weight vector, and the signal-to-noise ratio of the correction reference signal received by the receiving end RRU can be adjusted on the basis of changing the weight vector.

With reference to the first aspect, in some implementation manners of the first aspect, the selectable sets include at least one selectable set subset, where the selectable set subset includes transmission power and weight vectors that can be used when the first RRU is used as a sending end to send a calibration reference signal through an antenna, and transmission power and weight vectors that can be used when the second RRU is used as a sending end to send a calibration reference signal through an antenna, and a first selectable set subset in the at least one selectable set subset includes the first transmission power, the first weight vector, the second transmission power, and the second weight vector.

According to the channel correction method provided by the embodiment of the application, the transmission power and the weight vector used by the sending end RRU to send the correction reference signal are included in the first optional set subset, that is, the transmission power and the weight vector used by the sending end RRU to send the correction reference signal can be determined by determining the optional set subset, so that the accuracy of calculation of the correction coefficient is improved. And the first optional set subset is selected from at least one optional set subset, where the multiple optional set subsets include a transmission power and a weight vector that can be used when the sending end RRU sends the calibration reference signal, that is, when there are multiple optional set subsets, it is necessary to determine a first optional set subset from the multiple optional set subsets, and the sending end RRU sends the calibration reference signal to the receiving end RRU through its own antenna by using the transmission power and the weight vector included in the first optional set subset.

That is to say, in the embodiment of the present application, there may be multiple possibilities for the transmission power and the weight vector that can be used as the RRU to send the calibration reference signal, which increases the flexibility of the scheme.

With reference to the first aspect, in some implementations of the first aspect, the first selectable set subset corresponds to a first received power, a second received power, a third received power, a fourth received power, a signal-to-noise ratio of the fifth calibration reference signal, and a signal-to-noise ratio of the sixth calibration reference signal, where the first received power, the second received power, the third received power, and the fourth received power satisfy a preset power threshold, and the signal-to-noise ratio of the fifth calibration reference signal and the signal-to-noise ratio of the sixth calibration reference signal satisfy a preset signal-to-noise ratio threshold; wherein the first received power is a power of a calibration reference signal received at the first antenna, the second received power is a power of a calibration reference signal received at the second antenna, the third received power is a power of a calibration reference signal received at the third antenna, and the fourth received power is a power of a calibration reference signal received at the fourth antenna.

According to the channel correction method provided by the embodiment of the application, the selectable set subset can meet a certain preset condition, that is, the receiving power and the signal-to-noise ratio of the correction reference signal received by the receiving end RRU need to be considered in the process of determining the selectable set subset, that is, when the transmitting end RRU transmits the correction reference signal by using the transmission power and the weight vector included in the selectable set subset meeting the condition, the receiving power and the signal-to-noise ratio of the correction reference signal received by the receiving end RRU can be ensured to meet the requirement, so that the problem that the receiving and transmitting channel correction between the RRUs cannot be realized due to the fact that the signal-to-noise ratio of the correction reference signal received by the receiving end RRU is too.

Specifically, in this embodiment of the present application, determining the subset of the optional sets that meet the requirement may be determining the subset of the optional sets that is composed of a third transmit power, a third weight vector, a fourth transmit power, and a fourth weight vector that meet the requirement by traversing the transmit power in the first transmit power set, the weight vector in the first weight vector set, the transmit power in the second transmit power set, and the weight vector in the second weight vector set. The third transmit power, the third weight vector, the fourth transmit power, and the fourth weight vector may correspond to the first transmit power, the first weight vector, the second transmit power, and the second weight vector, or may correspond to other transmit powers in the first transmit power set, other weight vectors in the first weight vector set, other transmit powers in the second transmit power set, and other weight vectors in the second weight vector set. That is, there may be multiple subsets of the selectable sets that satisfy the requirement, where the traversal process may be: and determining whether the receiving power and the signal-to-noise ratio of the correction reference signal received by the corresponding receiving end meet the requirements or not, wherein the optional subset consists of any transmitting power in the first transmitting power set, any weight vector in the first weight vector set, any transmitting power in the second transmitting power set and any weight vector in the second weight vector set.

With reference to the first aspect, in certain implementations of the first aspect, the method further includes: the first RRU calculates the signal-to-noise ratio of the sixth correction reference signal; or the first RRU calculates a signal-to-noise ratio of a corrected reference signal obtained by combining the corrected reference signals received by the first antenna and the second antenna based on each weight vector in the first weight vector set, where the corrected reference signal obtained by combining based on the weight vectors is obtained by multiplying the corrected reference signals received by the first antenna and the second antenna by weights corresponding to the first antenna and the second antenna in the weight vectors, respectively, and adding the multiplication results.

According to the channel correction method provided in the embodiment of the present application, after a receiving end RRU receives a calibration reference signal sent by a sending end RRU, the calibration reference signal received on at least one antenna needs to be combined into one path of calibration reference signal and a signal-to-noise ratio of the combined calibration reference signal is calculated. Specifically, the receiving end RRU calculates the signal-to-noise ratio of the combined calibration reference signal, which may be only calculating the signal-to-noise ratio of the calibration reference signal after combining the weight vectors used by the current receiving end RRU as the sending end RRU to send the calibration reference signal; or, the receiving end RRU may calculate the combined calibration reference signals according to each weight vector in the weight vector set of the receiving end RRU, and calculate the signal-to-noise ratio of each combined calibration reference signal, where the calibration reference signals are received on at least two antennas in the receiving end.

That is to say, after the at least two antennas in the receiving end RRU receive the calibration reference signal, when the receiving end RRU calculates the combined calibration reference signal, the receiving end RRU may traverse each weight vector in its own weight vector set to respectively calculate the combined calibration reference signal, and calculate the signal-to-noise ratio of the calibration reference signal combined with each weight vector, where multiple calculated signal-to-noise ratios may be cached locally, and may be obtained locally when a certain signal-to-noise ratio needs to be utilized.

With reference to the first aspect, in certain implementations of the first aspect, the signal-to-noise ratio of the fifth calibration reference signal and the signal-to-noise ratio of the sixth calibration reference signal that have the smaller median are the signal-to-noise ratios with the largest median of the plurality of signal-to-noise ratios, where the plurality of signal-to-noise ratios are the signal-to-noise ratios with the smaller median of the two signal-to-noise ratios corresponding to the plurality of selectable subset sets, respectively. The two signal-to-noise ratios corresponding to each selectable set subset in the plurality of selectable set subsets are signal-to-noise ratios of the corrected reference signals after the corrected reference signals received by the antennas of each RRU in the two RRUs are combined.

For example, when the transmitter sends the calibration reference signal to the receiver with the transmission power #1 and the weight vector #1, the signal-to-noise ratio of the calibration reference signal received on the antenna of the receiver based on the weight vector #2 is one of the two signal-to-noise ratios corresponding to the subset of the selectable set, and when the transmitter sends the calibration reference signal to the receiver with the transmission power #2 and the weight vector #2, the signal-to-noise ratio of the calibration reference signal received on the antenna of the receiver based on the weight vector #1 is the other of the two signal-to-noise ratios corresponding to the subset of the selectable set.

According to the method for channel correction provided by the embodiment of the present application, an optimal subset (a first optional set subset) may be selected from the multiple determined optional set subsets, where the optimal optional set subset includes the first transmit power, the first weight vector, the second transmit power, and the second weight vector, so as to improve correction performance.

It should be understood that the present application is not limited to selecting an optimal subset of the selectable sets, and may select a subset of the selectable sets arbitrarily among a plurality of subsets of the selectable sets that satisfy the requirement.

It should be understood that the terms "first" and "second" in the present application are used for distinguishing between the description and the claims, and should not be construed to limit the present application in any way. Wherein the first RRU and the second RRU only distinguish different RRUs. Specifically, when the first RRU is a sending end RRU, the second RRU is a receiving end RRU; and when the second RRU is a sending end RRU, the first RRU is a receiving end RRU.

In a second aspect, a first RRU is provided, which may be used to perform operations of the first RRU in the first aspect and any possible implementation manner of the first aspect. In particular, the means for channel correction comprising means (means) for performing the steps or functions described in the above first aspect may be the first RRU. The steps or functions may be implemented by software, or hardware, or by a combination of hardware and software.

In a third aspect, a second RRU is provided, which may be configured to perform the operations of the second RRU. Specifically, the means (means) for channel correction including the steps or functions for performing the second RRU may be the second RRU. The steps or functions may be implemented by software, or hardware, or by a combination of hardware and software.

In a fourth aspect, there is provided an apparatus for channel correction, comprising a processor, a transceiver, and a memory, wherein the memory is used to store a computer program, the transceiver is used to execute the transceiving steps in the method for channel correction in any one of the possible implementations of the first aspect, and the processor is used to call and execute the computer program from the memory, so that the apparatus for channel correction executes the method for channel correction in any one of the possible implementations of the first aspect.

Optionally, there are one or more processors and one or more memories.

Alternatively, the memory may be integrated with the processor, or provided separately from the processor.

Optionally, the transceiver comprises a transmitter (transmitter) and a receiver (receiver).

In a fifth aspect, a system is provided, which comprises the apparatus for channel correction provided in the second and third aspects.

In a sixth aspect, there is provided a computer program product comprising: computer program (also called code, or instructions), which when executed, causes a computer to perform the method of any of the possible implementations of the first aspect described above.

In a seventh aspect, a computer-readable medium is provided, which stores a computer program (which may also be referred to as code or instructions) that, when executed on a computer, causes the computer to perform the method of any one of the possible implementations of the first aspect.

In an eighth aspect, a chip system is provided, which includes a memory for storing a computer program and a processor for calling and running the computer program from the memory, so that a communication device in which the chip system is installed executes the method in any one of the possible implementation manners of the first aspect.

The channel correction method and device provided by the embodiment of the application enable the sending end RRU to send the correction reference signal through at least two antennas and at least two antennas in the power and weight vector receiving end RRU, and can avoid the situation that the receiving and sending channel correction between the two RRUs cannot be corrected due to too low signal-to-noise ratio or too high power of the correction reference signal received by the receiving end RRU, thereby improving the receiving and sending channel correction performance between the RRUs.

Drawings

Fig. 1(a) and (b) are views to which the method of channel correction provided in the embodiment of the present application can be applied.

Fig. 2 is a schematic diagram of a connection structure between a BBU and an RRU according to an embodiment of the present application.

FIG. 3 is a schematic diagram of a method of channel correction.

FIG. 4 is a schematic diagram of another method of channel correction.

Fig. 5 is a schematic flow chart of a method for channel correction according to an embodiment of the present application.

Fig. 6 is a schematic flow chart of another method for channel correction according to an embodiment of the present disclosure.

Fig. 7 is a flowchart of a method for applying channel correction according to an embodiment of the present application.

Fig. 8 is a flowchart of another method for applying channel correction according to an embodiment of the present disclosure.

Fig. 9 is a flowchart of another method for applying channel correction according to an embodiment of the present disclosure.

Fig. 10 is a schematic diagram of a first RRU provided in an embodiment of the present application.

Fig. 11 is a schematic structural diagram of a device for channel calibration suitable for use in an embodiment of the present application.

Fig. 12 is a schematic diagram of a second RRU provided in an embodiment of the present application.

Fig. 13 is a schematic structural diagram of another apparatus for channel calibration suitable for use in embodiments of the present application.

Detailed Description

The technical solution in the present application will be described below with reference to the accompanying drawings.

The technical scheme of the embodiment of the application can be applied to various communication systems, for example: code Division Multiple Access (CDMA) system, Wideband Code Division Multiple Access (WCDMA) system, General Packet Radio Service (GPRS), Long Term Evolution (LTE) system, LTE Frequency Division Duplex (FDD) system, LTE Time Division Duplex (TDD), universal mobile telecommunications system (universal mobile telecommunications system, UMTS), universal microwave access (WiMAX) communication system, future fifth generation (5 transmission, 5G) system or New Radio (NR), etc.

First, a scenario in which the method for channel correction provided in the embodiment of the present application can be applied is briefly described with reference to fig. 1. Fig. 1(a) is a scene diagram to which the method for channel correction provided in the embodiment of the present application is applied. Two RRUs are included (e.g., RRU #1 and RRU #2 shown in fig. 1 (a)), where the two RRUs are respectively assigned with different base station physical addresses, i.e., the physical distance between the two RRUs is relatively long. Fig. 1(b) is another scenario diagram to which the method for channel correction provided in the embodiment of the present application is applied. Two RRUs are included (e.g., RRU #1 and RRU #2 as shown in fig. 1 (b)), where the two RRUs are assigned the same base station physical address, i.e., the physical distance between the two RRUs is very close. Or, RRU #1 and RRU #2 shown in fig. 1(a) may be referred to as two non-co-sited RRUs; similarly, RRU #1 and RRU #2 shown in fig. 1(b) can be referred to as two RRUs sharing a station.

Specifically, RRU #1 includes two antennas (antenna #1 and antenna #2), where a transceiving channel #1 of antenna #1 includes a transmitting channel #1 and a receiving channel #1, and a transceiving channel #2 of antenna #2 includes a transmitting channel #2 and a receiving channel # 2; two antennas (antenna #3 and antenna #4) are included in RRU #2, a transceiving channel #3 of antenna #3 includes a transmitting channel #3 and a receiving channel #3, and a transceiving channel #4 of antenna #4 includes a transmitting channel #4 and a receiving channel # 4.

The channel correction method provided in the embodiment of the present application can be used for correcting a transceiving channel between RRU #1 and RRU # 2. For example, the channel responses of the transmission/reception channel #1 and the transmission/reception channel #3 are corrected so that the channel response ratios of the transmission/reception channel #1 and the transmission/reception channel #3 coincide with each other.

It should be understood that fig. 1 is only an example for illustrating the applicable scenarios of the embodiments of the present application, and the scope of the present application is not limited thereto. For example, the embodiment of the present application may be applied to channel correction between at least two RRUs, that is, the number of RRUs in fig. 1 may be more than two; for example, in the embodiment of the present application, the number of antennas in each RRU is not limited, that is, the number of antennas in the RRU in fig. 1 may be more than two.

The above briefly introduces a scenario to which the method for channel correction provided in the embodiment of the present application can be applied in conjunction with fig. 1. In order to facilitate understanding of the method for channel correction provided in the embodiments of the present application, a brief description will be given of several basic concepts involved in the embodiments of the present application.

1. RRU and BBU.

Fig. 2 is a schematic diagram of a connection structure between a BBU and an RRU according to an embodiment of the present application. The schematic structural diagram includes a Remote Radio Unit (RRU) 02 and a baseband unit (BBU) 01 connected to the RRU through an optical fiber. It should be understood that a plurality of RRUs may be connected to a BBU, wherein the RRUs include: the RRU comprises a radio frequency unit 021 and at least one antenna 022, a specific address, wherein the radio frequency unit includes a digital intermediate frequency module, a transceiver module, a power amplifier module, and a filtering module (a specific internal module is not shown in fig. 2), and in a general case, the RRU converts a baseband optical signal into a radio frequency signal at a remote end to amplify and transmit the radio frequency signal. The digital intermediate frequency module is used for modulation and demodulation, digital up-down frequency conversion, analog-to-digital (A/D) conversion and the like of optical transmission; the transceiver module completes the conversion from the intermediate frequency signal to the radio frequency signal; and then the radio frequency signal is transmitted out through the antenna port by the power amplification module and the filtering module.

The RRU has the working principle that: the baseband signal is transmitted to the antenna feeder by frequency conversion, filtering, radio frequency filtering and sending filtering after passing through a linear power amplifier. And filtering, low-noise amplifying, further radio frequency small signal amplifying and filtering and down-conversion are carried out on the received mobile terminal uplink signal in an uplink, and then analog-to-digital conversion, digital intermediate frequency processing and the like are completed.

It should be understood that in the embodiments of the present application, improvement on RRU hardware is not involved, so that the specific form of RRU is defined in the prior art, and is not described herein again. Specifically, the RRU is referred to as a Remote Radio Unit (RRU) in this application, which is only one possible name, for example, the RRU may also be referred to as a Radio Remote Unit (RRU).

The BBU may be formed by one or more boards, and the boards may jointly support a radio access network of a single access system (e.g., an LTE system or a 5G system), or may respectively support radio access networks of different access systems. The BBU01 also includes a memory 001 and a processor 002. The memory 001 is used to store the necessary instructions and data. The processor 002 is used to control the RRU to perform the necessary actions. However, the RRU is not limited in this application to be controlled by the BBU connected to the RRU, and the RRU may also have a corresponding processor to control the RRU to perform necessary actions. The memory 001 and the processor 002 may serve one or more boards. That is, the memory and processor may be provided separately on each board. Multiple boards may share the same memory and processor. In addition, each single board can be provided with necessary circuits. When Joint Transmission (JT) is implemented by a CoMP communication system, the BBU may control multiple RRUs to transmit downlink signals to the same terminal device through inter-cell cooperation, so as to improve the signal reception quality of the terminal device.

2. Reciprocity.

Reciprocity refers to the property that, in the case of a single stimulus, when the stimulus port and the response port interchange positions, the response does not change as a result of such interchange. Where reciprocity may also be referred to as reciprocity.

The receiving and sending channels between the RRUs meeting the reciprocity in the embodiment of the present application means that all antennas between every two RRUs meet the reciprocity, and the antenna meeting the reciprocity can be understood as that the ratio of the channel response of the receiving channel to the channel response of the sending channel in each receiving and sending channel corresponding to each antenna in a plurality of antennas is the same.

3. Co-sited and non co-sited.

Co-sited as referred to in this application refers to a base station co-sited system (BTS co-site system), i.e. the physical distance between multiple RRUs is close, for example, the physical distance between two RRUs within 20 meters is called that the two RRUs are co-sited; non-co-sited refers to a base station non-co-sited system, i.e. the physical distance between a plurality of RRUs is far, for example, the physical distance between two RRUs is greater than 20 meters, which means that the two RRUs are not co-sited.

4. The reference signal is corrected.

The calibration reference signal referred to in the present application includes any one of the following sequences:

a sounding signal sequence generated using a Zadoff-Chu sequence defined in LTE, or a Golay sequence defined in Institute of Electrical and Electronics Engineers (IEEE) 802.16e, or other signal sequences having cross-correlation defined between cells, and the like.

It should be understood that, in the embodiment of the present application, a specific form of the calibration reference signal is not limited, and the calibration reference signal in the existing method for transmitting and receiving channels between RRUs may be used, or the calibration reference signal in the subsequent development of communication technology can be used for performing the transmission and receiving channels between RRUs. Preferably, the calibration reference signal, when transmitted, may cover the entire operating bandwidth of the cell.

5. And (5) correcting online.

The reciprocity correction of the transmit-receive channels between the RRUs referred to in this application is an on-line correction, which means that the correction is needed during use. The online correction corresponds to an offline correction, and the offline correction refers to a correction completed in factory shipment.

6、CSI。

In a Time Division Duplex (TDD) and multiple antenna (MIMO) system, a plurality of network devices using a CoMP technology receive an uplink Sounding Reference Signal (SRS) sent by a terminal device, and each network device obtains CSI of each antenna in each network device. The network equipment adopts the uplink CSI to jointly design downlink transmitting weight values of all antennas in all the network equipment based on reciprocity of the uplink CSI and the downlink CSI, so that space diversity gain and space multiplexing gain are obtained. In a multi-antenna system, transmit diversity and receive diversity can provide a certain diversity gain, which is often used to combat multi-path fading. The data stream is divided into a plurality of sub-data streams at the transmitting end and transmitted from different antennas, so that the transmission rate can be improved without increasing the transmission power and bandwidth. This technique is called a spatial multiplexing (spatial multiplexing) technique, and the resulting increase in transmission rate is called a spatial multiplexing gain.

7. And (5) weight vectors.

The weight vector referred to in the present application is a weight vector selected from a limited set of weight vectors, and is generally selected in a traversal manner. The weight vector in the present application may be considered as a weight vector in a pre-configured weight vector set.

Specifically, the reference signal combining and correcting based on the weight vector in the embodiment of the present application refers to: the corrected reference signal value received by each antenna is respectively multiplied by the sum of the weights corresponding to each antenna in the weight vector; the sending of the calibration reference signal based on the weight vector in the embodiment of the present application refers to: the calibration reference signal sent by each antenna is a calibration reference signal obtained by multiplying a preset calibration reference signal by a weight corresponding to each antenna in the weight vector.

8. Coherence time.

The coherence time is the maximum time difference range of the channel keeping constant, the same signal of the transmitting end reaches the receiving end within the coherence time, the fading characteristics of the signals are completely similar, and the receiving end is regarded as a signal.

The foregoing describes a scenario in which the method for channel correction provided by the embodiments of the present application can be applied, and some basic concepts involved. With the growing commercialization of fifth generation mobile communication systems, network devices are beginning to adopt massive multiple antenna (MIMO) technology, i.e., tens to hundreds of antennas are deployed on the same network device. The massive MIMO technology can fully utilize the spatial dimension of a wireless channel, significantly improve the cell capacity, and has become a key technology of a fifth generation mobile communication system. The large-scale MIMO technology can be fused with the CoMP technology, so that the rate of cell edge users is further improved, and the borderless cell experience with terminal equipment as the center is realized.

In order to facilitate understanding of the advantages of the method for channel correction provided by the embodiment of the present application compared with the existing method for channel correction, two existing methods for channel correction and the defects of the existing methods for channel correction are first described with reference to fig. 3 and 4.

FIG. 3 is a schematic diagram of a method of channel correction. The two antennas are included in RRU #1 and RRU #2, wherein RRU #1 includes two antennas (antenna #1 and antenna #2), and RRU #2 includes two antennas (antenna #3 and antenna # 4).

Specifically, in the channel correction method shown in fig. 3, each RRU uses a single antenna to complete the transceiver channel correction between the RRUs. Mainly comprises three steps:

the method comprises the following steps: the transmit power is determined.

1) Antenna #1 of RRU #1 with power P_imThe calibration reference signal #1 is sent in decibel milliwatts (dBm). Wherein m is 0,1, …, L_i-1，L_iIs the number of transmit powers in RRU # 1. For a calibration reference signal #1 transmitted by an antenna #1 of RRU #1 at an mth transmission power value, an antenna #3 of RRU #2 receives the calibration reference signal #1, and RRU #2 determines whether the power and the signal-to-noise ratio of the received calibration reference signal #1 meet a first preset requirement, and determines at least one transmission power corresponding to the calibration reference signal #1 meeting the first preset requirement.

Wherein, the number of the transmission power in the RRU #1 may be a preset transmission power set, for example, the transmission power set is { -40dBm, -20dBm, 40dBm }, and then 4 calibration reference signals #1 are transmitted by the antenna # 1; the first preset requirement is preset in RRU #2, for example, the first preset requirement is that the power is smaller than a power threshold, the signal-to-noise ratio is greater than a signal-to-noise ratio threshold, where the power threshold and the signal-to-noise ratio threshold are two preset thresholds.

Specifically, when there are multiple transmission power values corresponding to the calibration reference signal #1 meeting the first preset requirement, the RRU #2 selects an appropriate P from the multiple transmission power values_imValue, is recorded asWhen the first preset requirement is not metWhen the transmission power value corresponding to the correction reference signal #1 is obtained, the RRU #2 judges that the RRU #1 is not communicated with the RRU #2, and channel correction between the RRU #1 and the RRU #2 cannot be performed. For example, RRU #2 judges whether the power and signal-to-noise ratio of a corrected reference signal #1 respectively transmitted by an antenna #1 at the power of-20 dBm and 20dBm meet a first preset requirement, and RRU #2 selects 20dBm as the power value of-20 dBm and 20dBm

2) Antenna #3 of RRU #2 with power P_jndBm sends the corrected reference signal # 2. Wherein n is 0,1, …, L_j-1，L_jIs the number of transmit powers in RRU # 2. For the calibration reference signal #2 transmitted by the antenna #3 of the RRU #2 at the nth transmission power value, the antenna #1 of the RRU #1 receives the calibration reference signal #2, and the RRU #1 determines whether the power and the signal-to-noise ratio of the received calibration reference signal #2 satisfy the second preset requirement.

Antenna #1 of RRU #1 is powered by power P_imThe transmission of the corrected reference signal #1 is similar. The number of the transmission powers in RRU #2 may be a preset transmission power set, for example, the transmission power set is { -60dBm, -40dBm, 60dBm }, and then 4 calibration reference signals #2 are transmitted by the antenna # 3; the second preset requirement is preset in RRU #1, and is similar to the first preset requirement, and is not described herein again.

Specifically, when there are multiple transmission power values corresponding to the calibration reference signal #2 meeting the second preset requirement, the RRU #1 selects a suitable P from the multiple transmission power values_jnValue, is recorded asWhen there is no second transmission power value corresponding to the calibration reference signal #2 meeting the preset requirement, the RRU #1 judges that the RRU #1 and the RRU #2 are not communicated, and channel calibration cannot be performed between the RRU #1 and the RRU # 2.

Step two: and calculating a correction coefficient.

1) Antenna #1 of RRU #1 with power

Sending a correction reference signal #1 to an antenna #3 in the RRU #2, wherein the correction reference signal received by the antenna #3 is a correction reference signal # 1';

2) antenna #3 of RRU #2 with powerSending a correction reference signal #2 to an antenna #1 in the RRU #1, wherein the correction reference signal received by the antenna #1 is a correction reference signal # 2';

3) the correction coefficient is calculated based on the corrected reference signal #1 'received by the antenna #3 of RRU #2 and the corrected reference signal # 2' received by the antenna #1 of RRU # 1. Illustratively, calculating the correction coefficient includes:

calculating a first ratio of the receiving corrected reference signal #2 'of the antenna #1 to the transmitting corrected reference signal #2 of the antenna #3 and a second ratio of the receiving corrected reference signal # 1' of the antenna #3 to the transmitting corrected reference signal #1 of the antenna #1, and dividing the first ratio by the second ratio to obtain a correction coefficient of a channel response ratio of a transceiving channel of the antenna #1 to a transceiving channel of the antenna # 3.

Step three: and (6) channel correction.

And correcting the channel response of the transceiving channel between the RRU #1 and the RRU #2 through the correction coefficient so as to enable the channel response ratio of the transceiving channel between the RRU #1 and the RRU #2 to be consistent. For example, when the channel response ratio of the transceiving channel of RRU #2 is used as a reference value, the channel response of the transceiving channel of RRU #1 may be multiplied by the correction coefficient; or, dividing the channel response of the RRU #1 receiving channel by the correction coefficient; when the channel response ratio of the receiving and transmitting channel of the RRU #1 is used as a reference value, the channel response of the receiving and transmitting channel of the RRU #2 can be multiplied by the correction coefficient; alternatively, the channel response of the RRU #2 receive channel is divided by the correction coefficient.

However, the method of channel correction shown in fig. 3 has the following drawbacks:

1. in a non-co-located scene (the physical distance between RRU #1 and RRU #2 is long), there is a problem that the calibration reference signal #2 received by the antenna #1 and/or the signal-to-noise ratio of the calibration reference signal #1 received by the antenna #3 is too low to be calibrated. This is because the physical location between RRU #1 and RRU #2 is far away, the propagation loss of the electromagnetic wave air interface is large, and the signal-to-noise ratio of the received calibration reference signal will be low, which may cause the problem of being unable to calibrate. Particularly, when the network device adopts a large-scale MIMO technology, the RRU will adopt a large-scale antenna array, the transmission power on a single antenna in the RRU is correspondingly reduced, and the signal-to-noise ratio of the received calibration reference signal will be lower;

2. in a co-sited scene (the physical distance between RRU #1 and RRU #2 is very close), there is a problem that the power of the calibration reference signal #2 received by the antenna #1 and/or the power of the calibration reference signal #1 received by the antenna #3 is too high to be calibrated. There is a lower limit to the RRU transmit power at the calibration time, and even if the minimum transmit power is used, there is still a problem that the received calibration reference signal power is too high due to the close physical location, which may cause the Analog Automatic Gain Control (AAGC) to be initiated and not calibrated.

FIG. 4 is a schematic diagram of another method of channel correction. The two antennas are included in RRU #1 and RRU #2, wherein RRU #1 includes two antennas (antenna #1 and antenna #2), and RRU #2 includes two antennas (antenna #3 and antenna # 4).

Specifically, in the channel correction method shown in fig. 4, RRU #1 uses dynamic weights, and RRU #2 uses a single antenna to complete the transceiver channel correction between the RRUs. The dynamic weight value is obtained by on-line calculation and mainly comprises three steps:

the method comprises the following steps: and acquiring a dynamic weight.

Antenna #1 of RRU #1 sends correction reference signal #1 with default power for antenna #1 of RRU #1 to send correction reference signal #1 with default power, antenna # k of RRU #2 receives correction reference signal #1, and RRU #2 estimates that the air interface channel coefficients of antenna #1 of RRU #1 to antenna # k of RRU #2 are α_k. When RRU #1 and RRU #2 carry out channel correction, the dynamic weight w of the antenna # k of RRU #2_k＝(α_k)^*Wherein, the superscript indicates taking conjugate operation.

Step two: and calculating a correction coefficient.

1) Antenna #1 of RRU #1 transmits the calibration reference signal #1 with default power, and antenna #3 and antenna #4 of RRU #2 both transmit with default powerThe corrected reference signal #1 is received. And the RRU #2 obtains a path of corrected reference signal # 1' after weighting and summing the corrected reference signals #1 respectively received by the antenna #3 and the antenna #4, wherein the weighting coefficient is a dynamic weight value obtained by calculation in the step one. For example, antenna #3 corresponds to a weighting factor of w₃The weighting factor for antenna #4 is w₄。

2) Antenna #3 and antenna #4 of RRU #2 simultaneously transmit the calibration reference signal #2 at default power, respectively, and specifically, when antenna #3 and antenna #4 transmit the calibration reference signal #2, respectively, the calibration reference signal #2 transmitted by antenna #3 is multiplied by a weighting coefficient w₃Multiplying the corrected reference signal #2 transmitted from the antenna #4 by a weighting factor w₄. Antenna #1 of RRU #1 receives the corrected reference signal # 2'.

3) The correction coefficient is calculated based on the corrected reference signal #1 'received by RRU #2 and the corrected reference signal # 2' received by antenna #1 of RRU # 1. Illustratively, calculating the correction coefficient includes:

and calculating a first ratio of the corrected reference signal #2 'to the corrected reference signal #2 and a second ratio of the corrected reference signal # 1' to the corrected reference signal #1, and dividing the first ratio by the second ratio to obtain a correction coefficient for channel response correction of the transceiving channel between the RRU #1 and the RRU # 2.

Step three: and (6) channel correction.

And correcting the channel response of the transceiving channel between the RRU #1 and the RRU #2 through the correction coefficient so as to enable the channel response ratio of the transceiving channel between the RRU #1 and the RRU #2 to be consistent. For example, the channel response of the transmit channel may be multiplied by a correction coefficient; alternatively, the channel response of the receive channel is divided by the correction factor.

However, the method of channel correction shown in fig. 4 has the following drawbacks:

1. in a co-located scene (the physical distance between RRU #1 and RRU #2 is very close), there is a problem that the calibration reference signal #2 received by RRU #1 and/or the calibration reference signal #1 received by RRU #2 has too high power to be corrected. When the calibration reference signal is transmitted, transmission power traversal is not performed, the calibration reference signal is only transmitted by a default value, and after a dynamic weight is obtained, the power of the received calibration reference signal is obviously increased, which can cause AAGC (amplitude versus frequency) control starting and cannot be calibrated;

2. the dynamic weight calculation cost is large. The dynamic weight value coherence time is short, and in the worst case, the dynamic weight value at the current moment needs to be obtained before each correction, so that the complexity of the correction scheme is high, and the time overhead of the correction is large. Especially for a large-scale MIMO system, the dynamic wave beam is narrow, and the dynamic weight needs to be recalculated when the channel space gain direction changes.

3. The beam gain of RRU #1 is not utilized.

In order to solve the defects of the channel correction methods shown in fig. 3 and fig. 4, embodiments of the present application provide a channel correction method, which performs transmit-receive channel correction between RRUs by jointly traversing a transmit power set and a traversal weight set and selecting appropriate transmit power and weight, so as to improve performance of correcting the transmit-receive channel between RRUs. The method for channel calibration provided by the embodiment of the present application is described in detail below with reference to fig. 5 to 9.

Fig. 5 is a schematic flowchart of a method for channel correction according to an embodiment of the present application, including a first RRU, a second RRU, and steps S110 to S140. The first RRU comprises a first antenna and a second antenna, the second RRU comprises a third antenna and a fourth antenna, and each antenna has a corresponding transceiving channel.

S110, the first RRU sends the first correction reference signal and the second correction reference signal to the second RRU.

The first RRU and the second RRU are any two RRUs in a communication system comprising at least two RRUs. The channel correction method provided in the embodiment of the present application can be applied to correction of a transceiver channel between every two RRUs in a plurality of RRUs, and this embodiment is described by taking two RRUs (a first RRU and a second RRU) as an example only for convenience of description, and a transceiver channel correction procedure between every two RRUs in the plurality of RRUs is similar to a transceiver channel correction procedure between the two RRUs, and is not described in detail herein.

The first RRU includes a first antenna and a second antenna, and the second RRU includes a third antenna and a fourth antenna, which are examples and should not be limited in any way in this application. The RRU in this embodiment of the present application may include more than two antennas, where multiple antennas all transmit and/or receive the calibration reference signal, or at least two antennas of the multiple antennas transmit and/or receive the calibration reference signal, which will be described below with reference to a specific embodiment and will not be described herein again.

It is to be understood that the descriptions of "first," "second," and "third," etc. in this application are for purposes of distinction only and are not intended to be limiting. For example, the "first" and "second" of the first RRU and the second RRU are only used to distinguish different RRUs; the "first" and "second" of the first antenna and the second antenna are merely for distinguishing the different antennas.

Specifically, the first RRU sends a first correction reference signal to a third antenna and a fourth antenna in the second RRU through a first antenna in the first RRU with a first transmit power and a first weight vector, and the first RRU sends a second correction reference signal to the third antenna and the fourth antenna in the second RRU with the first transmit power and the first weight vector through a second antenna in the first RRU. The first transmit power is a transmit power in a first transmit power set in the first RRU, and the first weight vector is a weight vector in a first weight vector set in the first RRU.

The magnitude and the number of the transmission power included in the first transmission power set may be preset values according to the capability of the first RRU, and the first weight vector set may be a vector set designed by a developer, or may utilize vectors in an existing protocol. That is, in the embodiment of the present application, the merging of the first transmit power set and the first weight vector set is not limited, and may be existing multiplexing or redesigned.

Specifically, the first weight vector includes two elements, which correspond to the first antenna and the second antenna, respectively. A first correction reference signal sent by the first RRU through the first antenna is a correction reference signal obtained by multiplying a preset correction reference signal by a weight corresponding to the first antenna in the first weight vector; similarly, the second calibration reference signal sent by the first RRU via the second antenna is obtained by multiplying the preset calibration reference signal by the weight corresponding to the second antenna in the first weight vector. Wherein, the weight corresponding to the first antenna in the first weight vector is a non-0 element, and the weight corresponding to the second antenna in the first weight vector is also a non-0 element.

Specifically, when the weight corresponding to the first antenna in the first weight vector is 0, it indicates that the first antenna does not transmit the first calibration reference signal.

It should be understood that, in this application, a first antenna and a second antenna included in a first RRU are taken as an example for description, if the first RRU includes X antennas (X is an integer greater than or equal to 2), the first RRU may send, through each antenna of the X antennas, a calibration reference signal to a third antenna and a fourth antenna in the second RRU by using the first transmit power and the first weight vector, where the first weight vector includes X elements respectively corresponding to the X antennas, the calibration reference signal sent by each antenna is obtained by multiplying a preset calibration reference signal by a weight corresponding to the antenna in the first weight vector, and at least 2 elements in the X elements are nonzero.

As an example of the extension, the number of RRUs in a transceiver channel between RRUs to be corrected is N, and the numbers of the N RRUs are 0,1, …, and N-1, respectively. Specifically, the antenna in RRUi (i ═ 0,1, …, N-1) transmits powerAnd weight vectorSending a correction reference signal, wherein the weight value of a first correction reference signal transmitted on a k antenna in RRUi isThe k-th element of (a), wherein,

for a set of transmit powers (P) in RRUi_imdBm，m＝0,1,…,L_i-a transmit power in 1) that satisfies a preset condition,is a set of weight vectors (w) in RRUi_ib，b＝0,1,…,B_i-weight vectors in 1) that satisfy a predetermined condition, L_iIs the number of transmitted powers in RRUi, B_iThe number of weight vectors in RRUi.

S120, the second RRU acquires a fifth calibration reference signal.

After the third antenna and the fourth antenna in the second RRU receive the calibration reference signal, respectively, the second RRU combines the calibration reference signals received at the third antenna and the fourth antenna into a fifth calibration reference signal.

Illustratively, the fifth corrected reference signal is a sum of the corrected reference signal received at the third antenna, the corrected reference signal obtained by multiplying the weight corresponding to the third antenna in the second weight vector, the corrected reference signal received at the fourth antenna, and the corrected reference signal obtained by multiplying the weight corresponding to the fourth antenna in the second weight vector.

Illustratively, the second weight vector includes two elements, which correspond to the third antenna and the fourth antenna, respectively.

It should be understood that, in the present application, the third antenna and the fourth antenna included in the second RRU are taken as an example for description, if the second RRU includes Y antennas (Y is an integer greater than or equal to 2), the Y antennas can all receive the calibration reference signal sent by the first RRU, and at this time, the second weight vector includes Y elements, which correspond to the Y antennas respectively. The third calibration reference signal is a sum of the first calibration reference signal received by each antenna in the Y antennas multiplied by the weight corresponding to the third calibration reference signal in the second weight vector.

As an example of spreading, transmit power is applied to antennas in RRUiAnd weight vector

Transmission correctionFor reference signals, the weight vector is multiplied by the corrected reference signals received by all antennas in RRUj (j is 0,1, …, N-1, and j ≠ i)

After the weights of each antenna are respectively corresponding, a path of correction reference signal is obtained by summing.

S130, the second RRU sends the third and fourth calibration reference signals to the first RRU.

Specifically, the second RRU sends a third calibration reference signal to the first antenna and the second antenna in the first RRU through a third antenna in the second RRU with a second transmission power and a second weight vector; and the second RRU sends a fourth correction reference signal to the first antenna and the second antenna in the first RRU through a fourth antenna in the second RRU by using the second transmission power and the second weight vector. The second transmit power is one transmit power in a second transmit power set in the second RRU, and the second weight vector is one weight vector in a second weight vector set in the second RRU.

The magnitude and the number of the transmission power included in the second transmission power set may be preset values according to the capability of the second RRU, and the second weight vector set may be a vector set designed by a developer, or may utilize vectors in an existing protocol. That is to say, in the embodiment of the present application, the second transmit power set and the second weight vector set are not limited, and may be existing multiplexing or redesigned.

Specifically, the second weight vector includes two elements, which correspond to the third antenna and the fourth antenna, respectively. A third correction reference signal sent by a third antenna is obtained by multiplying a preset correction reference signal by a weight corresponding to the third antenna in the second weight vector; similarly, a fourth calibration reference signal sent by a fourth antenna is obtained by multiplying a preset calibration reference signal by a weight corresponding to the fourth antenna in the second weight vector.

It should be understood that, in this application, a third antenna and a fourth antenna included in the second RRU are taken as an example for description, if the second RRU includes Y antennas (Y is an integer greater than or equal to 2), the second RRU may send, through each antenna in the Y antennas, a calibration reference signal to the first antenna and the second antenna in the first RRU by using the above-mentioned second transmission power and the second weight vector, where the second weight vector includes Y elements respectively corresponding to the Y antennas, at least 2 elements in the Y elements are nonzero, and the calibration reference signal sent by each antenna is obtained by multiplying a preset calibration reference signal by a weight corresponding to the second weight vector.

As an example of the extension, the number of RRUs in a transceiver channel between RRUs to be corrected is N, and the numbers of the N RRUs are 0,1, …, and N-1, respectively. In particular, the antennas in RRUj (j ═ 0,1, …, N-1) are at transmit power

And weight vectorSending a correction reference signal, wherein the weight value of a second correction reference signal transmitted on the l antenna in the RRUj is

The first element of (a), wherein,is a set of transmission powers (P) in RRUj_jndBm，n＝0,1,…,L_j-a transmit power in 1) that satisfies a preset condition,is a set of weight vectors (w) in RRUj_jd，d＝0,1,…,B_j-weight vectors in 1) that satisfy a predetermined condition, L_jIs the number of transmitted powers in RRUj, B_jThe number of weight vectors in RRUj.

S140, the first RRU acquires a sixth calibration reference signal.

After the first antenna and the second antenna in the first RRU receive the calibration reference signal respectively, the first RRU combines the calibration reference signals received at the first antenna and the second antenna into a sixth calibration reference signal.

Illustratively, the sixth calibration reference signal is a sum of the calibration reference signal received at the first antenna, the calibration reference signal obtained by multiplying the weight corresponding to the first antenna in the first weight vector by the calibration reference signal received at the second antenna, and the calibration reference signal obtained by multiplying the weight corresponding to the second antenna in the first weight vector by the calibration reference signal.

Illustratively, the first weight vector includes two elements, which correspond to the first antenna and the second antenna, respectively.

It should be understood that, in this application, a first antenna and a second antenna included in a first RRU are taken as an example for description, if the first RRU includes X antennas (X is an integer greater than or equal to 2), the first RRU may receive the above-mentioned calibration reference signal sent by the second RRU through each antenna of the X antennas, and at this time, the first weight vector includes X elements, which correspond to the X antennas respectively. The sixth calibration reference signal is a sum of the calibration reference signal received by each antenna of the X antennas multiplied by a weight corresponding to the sixth calibration reference signal in the first weight vector.

For example, to transmit power to the antennas in RRUjAnd weight vector

For transmitting the srs, the weight vector is multiplied by the srs received by all antennas in the RRUi (i ═ 0,1, …, N-1, and j ≠ i)

After the weights of each antenna are respectively corresponding, a path of correction reference signal is obtained by summing.

After the fifth calibration reference signal and the sixth calibration reference signal are obtained, the calibration coefficient of the transceiving channel between the first RRU and the second RRU can be calculated based on the fifth calibration reference signal and the sixth calibration reference signal.

It should be understood that the method for calculating the correction coefficient of the transceiving channel between the first RRU and the second RRU based on the two calibration reference signals in the present application is not involved, and may be a method for calculating the correction coefficient of the transceiving channel between the first RRU and the second RRU based on the two calibration reference signals, which is already known in the prior art, or may be another method for calculating the correction coefficient of the transceiving channel between the first RRU and the second RRU based on the two calibration reference signals, which is proposed in the development process of the communication technology.

It should also be understood that the execution subject of calculating the correction coefficient may be the first RRU or the second RRU or a BBU connected to the first RRU or a BBU connected to the second RRU, or other management device.

For completeness of a scheme, in the present application, taking an existing method for calculating a correction coefficient of a transceiving channel between a first RRU and a second RRU based on two correction reference signals as an example, how to calculate the correction coefficient after acquiring a fifth correction reference signal and a sixth correction reference signal in the present application is briefly described:

and calculating a first ratio of the correction reference signal received and combined by the first RRU and the correction reference signal sent by the second RRU, and a second ratio of the correction reference signal received and combined by the second RRU and the correction reference signal sent by the first RRU, and dividing the result of the first ratio by the second ratio to be used as a correction coefficient of the channel response ratio of the transceiving channel between the first RRU and the second RRU.

It should be understood that after obtaining the correction coefficients, the correcting the transceiving channel between the first RRU and the second RRU may include:

and correcting the channel response of the transceiving channels by the correction coefficient so as to enable the channel response ratio of the transceiving channels to be consistent. For example, the channel response of the transmit channel may be multiplied by a correction coefficient; alternatively, the channel response of the receive channel is divided by the correction factor.

Specifically, the first and second RRUs shown in fig. 5 may be RRUs #1 and #2 shown in fig. 1(a) described above, or the first and second RRUs shown in fig. 5 may be RRUs #1 and #2 shown in fig. 1(b) described above.

As an implementation, the first RRU can determine which transmit power in the first set of transmit powers to use and which weight vector in the first set of weight vectors to send the first calibration reference signal to an antenna in the second RRU; the second RRU can determine which of the second set of transmit powers to send the second correction reference signal with and which of the second set of weight vectors to send to the antenna in the first RRU.

Illustratively, there is an alternative set comprising at least one alternative subset of sets, and a first alternative subset of the at least one alternative subset of sets comprises the first transmit power, the first weight vector, the second transmit power, and the second weight vector described above.

It should be understood that the optional set subset referred to in the embodiments of the present application refers to a set including 4 elements of the transmission power and weight vector that can be used by the first RRU and the transmission power and weight vector that can be used by the second RRU; and an alternative set is a set that includes at least one subset of the alternative set. For example, the selectable set includes M elements, and 4 elements of the M elements constitute a subset of the selectable set.

Next, how to determine the above-mentioned optional sets before executing the method flow shown in fig. 5 is described in detail with reference to fig. 6, where it is assumed that the first transmit power set includes L1 transmit powers, the first weight vector set includes B1 weight vectors, the second transmit power set includes L2 transmit powers, and the second weight vector set includes B2 weight vectors, where L1, B1, L2, and B2 are positive integers. Specifically, in this embodiment of the present application, an execution subject for determining the selectable set is not limited, and the execution subject may be the first RRU or the second RRU or a BBU connected to the first RRU or a BBU connected to the second RRU or other devices, and in the present application, only by ensuring that whichever device determines the selectable set, the first RRU and the second RRU can send the correction reference signal that needs to be sent in the embodiment illustrated in fig. 5 according to the power and weight vector included in one of the selectable set subsets, for example, the first RRU and the second RRU may be notified of the result after the other device determines, and when the other device determines the selectable set, and needs to use the power and the signal-to-noise ratio of the correction reference signal received by the first RRU and the second RRU, the first RRU and the second RRU may send the corresponding power and the signal-to-noise ratio to the device.

Fig. 6 is a schematic flow chart of another method for channel correction according to an embodiment of the present disclosure. The method comprises a first RRU, a second RRU and steps S210-S250. The first RRU comprises a first antenna and a second antenna, and the second RRU comprises a third antenna and a fourth antenna.

S210, the first RRU sends a calibration reference signal to the second RRU.

Assume that the first transmit power set includes L1 transmit powers, and the first weight vector set includes B1 weight vectors.

In order to determine the first transmit power and the first weight vector, the first RRU sends L1 × B1 calibration reference signals to antennas in the second RRU through each antenna in the first RRU with L1 transmit powers and B1 weight vectors, respectively.

For example, the first RRU traverses B1 weight vectors with the 0 th transmit power value in the first transmit power set, then traverses B1 weight vectors with the 1 st transmit power value in the first transmit power set, and so on, …; the traversal of different transmitting power values is completed in a time division mode, and the traversal of different weight vectors can be completed in a time division, frequency division (combing) or code division mode; or, the antenna in the first RRU traverses L1 transmission powers with the 0 th weight vector in the first weight vector set, then traverses L1 transmission power amounts with the 1 st weight vector in the first weight vector set, and so on, …; the traversal of different weight vectors is completed in a time division mode, and the traversal of different transmitting powers can be completed in a time division, frequency division (combing) or code division mode; or a random traversal.

Exemplarily, the first RRU sends, through a first antenna and a second antenna in the first RRU, the calibration reference signal to the third antenna and the fourth antenna respectively by using a first transmit power and a first weight vector, where the first transmit power is any one of L1 transmit powers in the first transmit power set, and the first weight vector is any one of B1 weight vectors in the first weight vector set.

For example, the number of RRUs in the transceiver channel between RRUs to be corrected is N, and the numbers of the N RRUs are 0,1, …, and N-1, respectively. Antenna in RRUi (i-0, 1, …, N-1) with power P_imdBm and weight vector w_ibTransmitting a correction reference signal to an antenna in RRUj (j is 0,1, …, N-1 and j is not equal to i), wherein the weight value of the correction reference signal transmitted on the k-th antenna in RRUi is w_ibWherein m is 0,1, …, L_i-1，b＝0,1,…,B_i-1，L_iIs the number of transmission powers in the first set of transmission powers in the RRUi, B_iThe number of the weight vectors in the first weight vector set in the RRUi.

S220, the second RRU sends a calibration reference signal to the first RRU.

Assume that the second transmit power set includes L2 transmit powers, and the second weight vector set includes B2 weight vectors.

In order to determine the second transmit power and the second weight vector, the second RRU sends L2 × B2 calibration reference signals to the antennas in the first RRU through each antenna in the second RRU with L2 transmit powers and B2 weight vectors, respectively.

For example, the second RRU traverses B2 weight vectors with the 0 th transmit power value in the second transmit power set, then traverses B2 weight vectors with the 1 st transmit power value in the second transmit power set, and so on, …; the traversal of different transmitting power values is completed in a time division mode, and the traversal of different weight vectors can be completed in a time division, frequency division (combing) or code division mode; or the antenna in the second RRU traverses L2 transmission powers by using the 0 th weight vector in the second weight vector set, then traverses L2 transmission power amounts by using the 1 st weight vector in the second weight vector set, and so on, …; the traversal of different weight vectors is completed in a time division mode, and the traversal of different transmitting powers can be completed in a time division, frequency division (combing) or code division mode; or a random traversal.

Exemplarily, the second RRU sends, through a third antenna and a fourth antenna in the second RRU, a correction reference signal to the first antenna and the second antenna respectively by using a second transmission power and a second weight vector, where the second transmission power is any one of L2 transmission powers in the second transmission power set, and the second weight vector is any one of B2 weight vectors in the second weight vector set.

For example, the number of RRUs in the transceiver channel between RRUs to be corrected is N, and the numbers of the N RRUs are 0,1, …, and N-1, respectively. Antenna in RRUj (j is 0,1, …, N-1) with power P_jndBm and weight vector w_jdTransmitting a calibration reference signal to antennas in RRUi (i ═ 0,1, …, N-1, and j ≠ i), with weight w on the l-th antenna in RRUj_jdWherein n is 0,1, …, L_j-1，d＝0,1,…,B_j-1，L_jIs the number of transmission powers in the second set of transmission powers in RRUj, B_jThe number of the weight vectors in the second weight vector set in RRUj.

S230, determining the selectable set subset.

For example, when the first RRU sends the calibration reference signal to the third antenna and the fourth antenna in the second RRU respectively through the first antenna and the second antenna in the first RRU with the transmission power 1 in the first transmission power set and the weight vector 1 in the first weight vector set, and the second RRU sends the calibration reference signal to the first antenna and the second antenna in the first RRU respectively through the third antenna and the fourth antenna in the second RRU with the transmission power 2 in the second transmission power set and the weight vector 2 in the second transmission power set. It can be considered that the transmit power 1, weight vector 1, transmit power 2 and weight vector 2 constitute a potentially selectable subset of the set.

The potential optional set subset corresponds to received power 1, received power 2, received power 3, received power 4, signal-to-noise ratio 1 and signal-to-noise ratio 2, and the condition that the potential optional set subset needs to satisfy is that: the received power 1, the received power 2, the received power 3 and the received power 4 meet a preset power threshold, and the signal-to-noise ratio 1 and the signal-to-noise ratio 2 meet a preset signal-to-noise ratio threshold. Wherein, the received power 1 corresponding to the potential selectable set subset is the power of the calibration reference signal received at the first antenna, the received power 2 is the power of the calibration reference signal received at the second antenna, the third received power 3 is the power of the calibration reference signal received at the third antenna, the fourth received power 4 is the power of the calibration reference signal received at the fourth antenna, the signal-to-noise ratio 1 is the signal-to-noise ratio of the calibration reference signal obtained after combining the calibration reference signals received at the first antenna and the second antenna based on the weight vector 1, and the signal-to-noise ratio 2 is the signal-to-noise ratio of the calibration reference signal obtained after combining the calibration reference signals received at the third antenna and the fourth antenna based on the weight vector 2.

As can be seen from the above-mentioned condition that needs to be satisfied for the subset of the potential selectable sets, the condition needs to be satisfied for the subset of the first selectable set including the first transmit power, the first weight vector, the second transmit power, and the second weight vector. Specifically, the method comprises the following steps:

the first selectable set subset corresponds to a first receiving power, a second receiving power, a third receiving power, a fourth receiving power, a signal-to-noise ratio of a fifth correction reference signal and a signal-to-noise ratio of a sixth correction reference signal, the first receiving power, the second receiving power, the third receiving power and the fourth receiving power meet a preset power threshold, and the signal-to-noise ratio of the fifth correction reference signal and the signal-to-noise ratio of the sixth correction reference signal meet a preset signal-to-noise ratio threshold;

wherein the first received power is a power at which the calibration reference signal is received at the first antenna, the second received power is a power at which the calibration reference signal is received at the second antenna, the third received power is a power at which the calibration reference signal is received at the third antenna, and the fourth received power is a power at which the calibration reference signal is received at the fourth antenna.

For example, toThe above embodiment is extended, and for the calibration reference signal transmitted by the RRUi with the mth transmission power value and the mth weight vector, the power of the calibration reference signal received by the antenna l of the RRUj (j is 0,1, …, N-1, and j is not equal to i) is denoted as the calibration Reference Signal Received Power (RSRP), RSRP_imb,jlRRUj bases the corrected reference signals received on all antennas on weight vector w_jdCombining into a correction reference signal, and recording the signal-to-noise ratio of the correction reference signal as SNR_imb,jdWherein the weight on the first antenna is w_jdThe l element of (1); for the corrected reference signal transmitted by RRUj with the nth transmission power value and the d weight vector, the power of the corrected reference signal received on antenna k of RRUi (i ═ 0,1, …, N-1, and j ≠ i) is denoted as RSRP_jnd,ikRRUi bases the corrected reference signals received on all antennas on the weight vector w_ibCombining into a correction reference signal, and recording the signal-to-noise ratio of the correction reference signal as SNR_jnd,ibWherein the weight on the kth antenna is w_ibThe kth element of (1).

Wherein when RSRP is satisfied_imb,jl<Th_Upper，RSRP_jnd,ik<Th_Upper，SNR_imb,jd>Th_Lower，SNR_jnd,ib>Th_LowerThe first transmit power, the first weight vector, the second transmit power and the second weight vector { P } corresponding to the four formulas_im，w_ib，P_jn，w_jdForm a subset C of the alternative set_imb,jndWherein, Th_UpperIndicating an upper limit value, Th, of the received corrected reference signal power_LowerA lower limit value representing the signal-to-noise ratio of the received correction reference signal, l being w_jdThe number of the middle element being nonzero, k being w_ibThe non-zero sequence number of the middle element. If there is no optional subset, RRUi and RRUj are not connected, and correction cannot be carried out.

Exemplarily, before S230, fig. 5 further includes: s221, calculating a signal-to-noise ratio of the sixth calibration reference signal; and S222, calculating the signal-to-noise ratio of the fifth correction reference signal.

Illustratively, the performing body for calculating the signal-to-noise ratio of the sixth correction reference signal may be the first RRU, or a BBU to which the first RRU is connected, or other management device.

Specifically, the calculating of the signal-to-noise ratio of the sixth corrected reference signal may be after the first antenna and the second antenna receive the corrected reference signal transmitted by the third antenna and the fourth antenna at the second transmission power and the second weight vector. Combining the correction reference signals received at the first antenna and the second antenna based on the first weight vector to obtain a sixth correction reference signal, and calculating the signal-to-noise ratio of the sixth correction reference signal; the corrected reference signals received at the first antenna and the second antenna can be combined to obtain combined corrected reference signals and the signal-to-noise ratio of the combined corrected reference signals can be calculated based on each weight vector in the first weight vector set.

Similarly, the calculating of the snr of the fifth calibration reference signal may be after the third antenna and the fourth antenna receive the calibration reference signal transmitted by the first antenna and the second antenna with the first transmit power and the first weight vector. Combining the correction reference signals received at the third antenna and the fourth antenna based on the second weight vector to obtain a fifth correction reference signal, and calculating the signal-to-noise ratio of the fifth correction reference signal; and combining the correction reference signals received at the third antenna and the fourth antenna based on each weight vector in the second weight vector set to obtain a combined correction reference signal, and calculating the signal-to-noise ratio of the combined correction reference signal.

It should be understood that the performing body of the above determining the selectable set subset may be the first RRU, e.g., the second RRU sends the calculated received corrected reference signal power and the received corrected reference signal to noise ratio to the first RRU; alternatively, the first and second electrodes may be,

the performing body of the above determining the selectable set subset may be a second RRU, for example, the first RRU sends the calculated received corrected reference signal power and the received corrected reference signal to noise ratio to the second RRU; alternatively, the first and second electrodes may be,

the implementation subject of the above determining the selectable set subset may be other management devices, for example, the first RRU sends the calculated incoming received corrected reference signal power and the received corrected reference signal to noise ratio to the management device and the second RRU sends the calculated incoming received corrected reference signal power and the received corrected reference signal to noise ratio to the management device.

Specifically, the optional set subset determined in S230 may include a plurality of optional sets. At this time, in order to determine the first transmit power, the first weight vector, the second transmit power and the second weight vector actually used by the first RRU and the second RRU in the embodiment shown in fig. 5, optionally, fig. 6 further includes S240, and the first optional set subset is determined.

A first subset of the selectable sets comprising the first transmit power, the first weight vector, the second transmit power, and the second weight vector is determined from a plurality of subsets of the selectable sets.

Optionally, determining a first selectable set subset including the first transmit power, the first weight vector, the second transmit power, and the second weight vector from a plurality of selectable set subsets includes the following two steps:

the method comprises the following steps: determining, from the plurality of selectable set subsets, a smaller value of two signal-to-noise ratios (for example, the two signal-to-noise ratios corresponding to one of the selectable set subsets may be signal-to-noise ratio 1 and signal-to-noise ratio 2 as described in the above embodiment) corresponding to the plurality of selectable set subsets, respectively, where the plurality of selectable set subsets exist in a plurality of smaller values;

step two: and selecting a selectable subset corresponding to the maximum value from the plurality of smaller values, wherein the selectable subset can be called a first selectable subset, and comprises first transmission power, a first weight vector, second transmission power and a second weight vector.

According to the process of determining the first selectable set subset shown in the first step and the second step, the signal-to-noise ratio of the fifth corrected reference signal corresponding to the first selectable set subset and the signal-to-noise ratio of the sixth corrected reference signal having the smaller median value are the signal-to-noise ratios having the largest median values of the plurality of signal-to-noise ratios, and the plurality of signal-to-noise ratios are the signal-to-noise ratios having the smaller median values of the two signal-to-noise ratios corresponding to the plurality of selectable set subsets, respectively.

Alternatively, one selectable set subset may be arbitrarily selected from among a plurality of selectable set subsets as the first selectable set subset described above.

As an implementation manner, if the selectable set subset determined in S230 includes only one, the selectable set subset is the first selectable set subset.

It should be understood that the execution of S230 and S240 by the first RRU in fig. 6 is only an example, and does not limit the scope of the present application in any way.

To facilitate understanding of the flow shown in fig. 6, a specific example is further described:

assume that a first set of transmit powers in a first RRU includes two transmit powers (transmit power #1 and transmit power # 2); a first weight vector set in the first RRU includes two weight vectors (a weight vector #1 and a weight vector #2), wherein each weight vector includes two elements, and the two elements respectively correspond to a first antenna and a second antenna in the first RRU;

the second set of transmit powers in the second RRU includes two transmit powers (transmit power #3 and transmit power # 4); the second weight vector set in the second RRU includes two weight vectors (weight vector #3 and weight vector #4), where each weight vector includes two elements, and corresponds to a third antenna and a fourth antenna in the second RRU, respectively.

Then, the flow shown in fig. 6 includes the following steps:

the method comprises the following steps: a first antenna and a second antenna in the first RRU send a first correction reference signal to the second RRU by using transmission power #1 and a weight vector # 1;

1) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #3 and the weight vector # 3;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #311, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 411; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on the weight vector #3 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 311;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #133, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 233; and combining the corrected reference signal received by the first antenna and the corrected reference signal received by the second antenna into a corrected reference signal based on the weight vector #1, and marking the signal-to-noise ratio of the combined corrected reference signal as SNR # 133.

Judging whether the RSRP #311, the RSRP #411, the RSRP #133 and the RSRP #233 meet a preset power threshold or not; whether the SNR #311 and the SNR #133 described above satisfy a preset signal-to-noise ratio threshold.

It is assumed that the RSRP #311, RSRP #411, RSRP #133, and RSRP #233 satisfy the predetermined power threshold; if the SNR #311 and the SNR #133 satisfy a predetermined SNR threshold, { transmission power #1, weight vector #1, transmission power #3, weight vector #3} is one of the above-mentioned candidate subsets;

2) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #3 and the weight vector # 4;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #311, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 411; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on a weight vector #4 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 411;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #134, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 234; and combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #1 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 134.

Judging whether the RSRP #311, the RSRP #411, the RSRP #134 and the RSRP #234 meet a preset power threshold or not; whether the SNR #411 and the SNR #134 satisfy the preset SNR threshold.

It is assumed that the RSRP #311, RSRP #411, RSRP #134, and RSRP #234 described above do not satisfy the preset power threshold; if the SNR #411 and the SNR #134 do not satisfy the predetermined SNR threshold, the { transmit power #1, the weight vector #1, the transmit power #3, the weight vector #4} does not belong to the subset of the alternative set;

3) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #4 and the weight vector # 3;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #311, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 411; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on the weight vector #3 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 311;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #143, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 243; and combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #1 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 143.

Judging whether the RSRP #311, the RSRP #411, the RSRP #143 and the RSRP #243 meet a preset power threshold or not; whether the SNR #311 and the SNR #143 satisfy a preset SNR threshold.

It is assumed that the RSRP #311, RSRP #411, RSRP #143, and RSRP #243 described above do not satisfy the preset power threshold; if the SNR #311 and the SNR #143 do not satisfy the predetermined SNR threshold, the { transmit power #1, the weight vector #1, the transmit power #4, the weight vector #3} does not belong to the subset of the selectable set;

4) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #4 and the weight vector # 4;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #311, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 411; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on a weight vector #4 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 411;

the corrected reference signal power received by the first antenna in the first RRU is denoted as RSRP #144, and the corrected reference signal power received by the second antenna in the first RRU is denoted as RSRP # 244; and combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #1 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 144.

Judging whether the RSRP #311, the RSRP #411, the RSRP #144 and the RSRP #244 meet a preset power threshold or not; whether the SNR #411 and the SNR #144 satisfy the preset SNR threshold.

It is assumed that the RSRP #311, RSRP #411, RSRP #144, and RSRP #244 described above do not satisfy the preset power threshold; if the SNR #411 and the SNR #144 do not satisfy the predetermined SNR threshold, the { transmit power #1, the weight vector #1, the transmit power #4, the weight vector #4} does not belong to the subset of the selectable set;

step two: a first antenna and a second antenna in the first RRU send a first correction reference signal to the second RRU by using transmission power #1 and a weight vector # 2;

1) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #3 and the weight vector # 4;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #312, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 412; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on a weight vector #4 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 412;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #134, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 234; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #2 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 234;

judging whether the RSRP #312, the RSRP #412, the RSRP #134 and the RSRP #234 meet a preset power threshold; whether SNR #412 and SNR #234 meet the predetermined signal-to-noise ratio threshold.

It is assumed that the RSRP #312, RSRP #412, RSRP #134, and RSRP #234 satisfy the predetermined power threshold; if the SNR #412 and the SNR #234 satisfy a predetermined SNR threshold, { transmit power #1, weight vector #2, transmit power #3, and weight vector #4} is a subset of the selectable set;

2) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #3 and the weight vector # 3;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #312, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 412; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on the weight vector #3 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 312;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #133, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 233; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #2 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 233;

judging whether the RSRP #312, the RSRP #412, the RSRP #133 and the RSRP #233 meet a preset power threshold or not; whether the SNR #312 and SNR #233 described above satisfy a preset signal-to-noise ratio threshold.

It is assumed that the RSRP #312, RSRP #412, RSRP #133, and RSRP #233 described above do not satisfy the preset power threshold; if the SNR #312 and the SNR #233 do not satisfy the predetermined SNR threshold, the { transmit power #1, the weight vector #2, the transmit power #3, the weight vector #3} does not belong to the subset of the selectable set;

3) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #4 and the weight vector # 3;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #312, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 412; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on the weight vector #3 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 312;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #143, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 243; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #2 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 243;

judging whether the RSRP #312, the RSRP #412, the RSRP #143 and the RSRP #243 meet a preset power threshold or not; whether the SNR #312 and SNR #243 meet the preset signal-to-noise ratio threshold.

It is assumed that the RSRP #312, RSRP #412, RSRP #143, and RSRP #243 described above do not satisfy the preset power threshold; if the SNR #312 and the SNR #243 do not satisfy the predetermined SNR threshold, the { transmit power #1, the weight vector #2, the transmit power #4, the weight vector #3} does not belong to the subset of the selectable set;

4) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #4 and the weight vector # 4;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #312, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 412; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on a weight vector #4 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 412;

the corrected reference signal power received by the first antenna in the first RRU is denoted as RSRP #144, and the corrected reference signal power received by the second antenna in the first RRU is denoted as RSRP # 244; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #2 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 244;

judging whether the RSRP #312, the RSRP #412, the RSRP #144 and the RSRP #244 meet a preset power threshold or not; whether the SNR #412 and the SNR #244 described above satisfy a preset signal-to-noise ratio threshold.

It is assumed that the RSRP #312, RSRP #412, RSRP #144, and RSRP #244 described above do not satisfy the preset power threshold; if the SNR #312 and the SNR #412 do not satisfy the predetermined SNR threshold, the { transmit power #1, the weight vector #2, the transmit power #4, the weight vector #4} does not belong to the subset of the alternative set;

step three: a first antenna and a second antenna in the first RRU send a first correction reference signal to the second RRU by using transmission power #2 and a weight vector # 1;

1) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #4 and the weight vector # 3;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #321, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 421; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on the weight vector #3 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 321;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #143, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 243; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #1 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 143;

judging whether the RSRP #321, the RSRP #421, the RSRP #143 and the RSRP #243 meet a preset power threshold; whether the SNR #321 and the SNR #143 satisfy a preset SNR threshold.

It is assumed that the RSRP #321, RSRP #421, RSRP #143, and RSRP #243 satisfy the predetermined power threshold; the SNR #321 and SNR #143 meet a predetermined SNR threshold, and { transmit power #2, weight vector #1, transmit power #4, weight vector #3} is one of the selectable subset;

2) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #3 and the weight vector # 3;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #321, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 421; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on the weight vector #3 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 321;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #133, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 233; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #1 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 133;

judging whether the RSRP #321, the RSRP #421, the RSRP #133 and the RSRP #233 meet a preset power threshold; whether the SNR #321 and the SNR #133 satisfy a preset SNR threshold.

It is assumed that the RSRP #321, RSRP #421, RSRP #133, and RSRP #233 described above do not satisfy the preset power threshold; if the SNR #321 and the SNR #133 do not satisfy the predetermined SNR threshold, the { transmit power #2, the weight vector #1, the transmit power #3, the weight vector #3} does not belong to the subset of the selectable set;

3) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #3 and the weight vector # 4;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #321, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 421; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on a weight vector #4 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 421;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #134, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 234; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #1 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 134;

judging whether the RSRP #321, the RSRP #421, the RSRP #134 and the RSRP #234 meet a preset power threshold; whether the SNR #421 and the SNR #134 satisfy the preset SNR threshold.

It is assumed that the RSRP #321, RSRP #421, RSRP #134, and RSRP #234 do not satisfy the predetermined power threshold; if the SNR #421 and the SNR #134 do not satisfy the predetermined SNR threshold, the { transmit power #2, the weight vector #1, the transmit power #3, the weight vector #4} does not belong to the subset of the selectable set;

4) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #4 and the weight vector # 4;

the corrected reference signal power received by a third antenna in the second RRU is denoted as RSRP #321, and the corrected reference signal power received by a fourth antenna in the second RRU is denoted as RSRP # 421; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on a weight vector #4 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 421;

the corrected reference signal power received by the first antenna in the first RRU is denoted as RSRP #144, and the corrected reference signal power received by the second antenna in the first RRU is denoted as RSRP # 244; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #1 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 144;

judging whether the RSRP #321, the RSRP #421, the RSRP #144 and the RSRP #244 meet a preset power threshold; whether the SNR #421 and SNR #144 satisfy the preset SNR threshold.

It is assumed that the RSRP #321, RSRP #421, RSRP #144, and RSRP #244 described above do not satisfy the preset power threshold; if the SNR #421 and SNR #144 do not satisfy the predetermined SNR threshold, the { transmit power #2, weight vector #1, transmit power #4, weight vector #4} does not belong to the subset of the selectable set;

step four: a first antenna and a second antenna in the first RRU send a first correction reference signal to the second RRU by using transmission power #2 and weight vector # 2;

1) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #4 and the weight vector # 4;

the power of a corrected reference signal received by a third antenna in the second RRU is denoted as RSRP #322, and the power of a corrected reference signal received by a fourth antenna in the second RRU is denoted as RSRP # 322; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on a weight vector #4 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 422;

the corrected reference signal power received by the first antenna in the first RRU is denoted as RSRP #144, and the corrected reference signal power received by the second antenna in the first RRU is denoted as RSRP # 244; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #2 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 244;

judging whether the RSRP #322, the RSRP #422, the RSRP #144 and the RSRP #244 meet a preset power threshold or not; whether SNR #422 and SNR #244 meet the predetermined signal-to-noise threshold.

It is assumed that the RSRP #322, RSRP #422, RSRP #144, and RSRP #244 described above satisfy the preset power threshold; if the SNR #422 and the SNR #244 satisfy a predetermined SNR threshold, { transmit power #2, weight vector #2, transmit power #4, weight vector #4} is a subset of the selectable set;

2) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #3 and the weight vector # 3;

the power of a corrected reference signal received by a third antenna in the second RRU is denoted as RSRP #322, and the power of a corrected reference signal received by a fourth antenna in the second RRU is denoted as RSRP # 322; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on the weight vector #3 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 322;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #133, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 233; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #2 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 233';

judging whether the RSRP #322, the RSRP #422, the RSRP #133 and the RSRP #233 meet a preset power threshold; whether the SNR #322 and SNR #233 described above satisfy a preset signal-to-noise ratio threshold.

It is assumed that the RSRP #322, RSRP #422, RSRP #133, and RSRP #233 described above do not satisfy the preset power threshold; if the SNR #322 and the SNR #233 do not satisfy the predetermined SNR threshold, the { transmit power #2, the weight vector #2, the transmit power #3, the weight vector #3} does not belong to the subset of the candidate set;

3) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #3 and the weight vector # 4;

the power of a corrected reference signal received by a third antenna in the second RRU is denoted as RSRP #322, and the power of a corrected reference signal received by a fourth antenna in the second RRU is denoted as RSRP # 322; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on a weight vector #4 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 422;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #134, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 234; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #2 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 234;

judging whether the RSRP #322, the RSRP #422, the RSRP #134 and the RSRP #234 meet a preset power threshold; SNR #422 and SNR #234, as described above, meet a pre-set signal-to-noise threshold.

It is assumed that the RSRP #322, RSRP #422, RSRP #134, and RSRP #234 described above do not satisfy the preset power threshold; if the SNR #422 and the SNR #234 do not satisfy the predetermined SNR threshold, the { transmit power #2, the weight vector #2, the transmit power #3, the weight vector #4} does not belong to the subset of the selectable set;

4) a third antenna and a fourth antenna in the second RRU send a second correction reference signal to the first RRU by using the transmission power #4 and the weight vector # 3;

the power of a corrected reference signal received by a third antenna in the second RRU is denoted as RSRP #322, and the power of a corrected reference signal received by a fourth antenna in the second RRU is denoted as RSRP # 322; combining the correction reference signal received by the third antenna and the correction reference signal received by the fourth antenna based on the weight vector #3 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 322;

the corrected reference signal power received by a first antenna in the first RRU is denoted as RSRP #143, and the corrected reference signal power received by a second antenna in the first RRU is denoted as RSRP # 243; combining the correction reference signal received by the first antenna and the correction reference signal received by the second antenna based on the weight vector #2 to obtain a path of correction reference signal, and marking the signal-to-noise ratio of the combined correction reference signal as SNR # 243;

judging whether the RSRP #322, the RSRP #422, the RSRP #143 and the RSRP #243 meet a preset power threshold or not; whether SNR #322 and SNR #243 meet the predetermined signal-to-noise ratio threshold.

It is assumed that the RSRP #322, RSRP #422, RSRP #143, and RSRP #243 described above do not satisfy the preset power threshold; if the SNR #322 and SNR #243 do not satisfy the predetermined SNR threshold, then { transmit power #2, weight vector #2, transmit power #4, weight vector #3} does not belong to the subset of the alternative set;

it should be understood that in this specific example, the set of transmit power and the set of weight vectors in the first RRU and the second RRU respectively include two elements. That is, the possible combinations of the corrected reference signals are transmitted to each other with different transmit powers and weight vectors: { the transmission power of the first RRU, the weight vector of the first RRU, the transmission power of the second RRU, and the weight vector of the second RRU } have 16 in total, which is called as 16 subsets.

Judging whether one subset is the optional subset according to the knowledge, wherein when the first RRU sends a correction reference signal to the second RRU according to the transmission power of the first RRU and the weight vector of the first RRU in each subset, whether the power of the correction reference signal received by each antenna in the second RRU meets a preset power threshold, and whether the signal-to-noise ratio of the correction reference signal obtained by combining the correction reference signal received by each antenna in the second RRU with the weight vector of the second RRU meets a preset signal-to-noise ratio threshold; and when the second RRU sends the correction reference signal to the first RRU by using the transmission power of the second RRU and the weight vector of the second RRU in each subset, whether the power of the correction reference signal received by each antenna in the first RRU meets a preset power threshold or not, and whether the signal-to-noise ratio of the correction reference signal obtained by combining the correction reference signals received by each antenna in the first RRU by using the weight vector of the first RRU meets a preset signal-to-noise ratio threshold or not are determined. The following briefly describes how to obtain the above-mentioned 6 measurements for each subset:

the first condition is as follows:

the 6 measurements corresponding to each subset are measured separately.

For example, RSRP #311, RSRP #411, RSRP #133, RSRP #233, SNR #311, and SNR #133 corresponding to the above-described subset { transmit power #1, weight vector #1, transmit power #3, weight vector #3 }; and RSRP #311, RSRP #411, RSRP #134, RSRP #234, SNR #411, and SNR #134 corresponding to the subset { transmit power #1, weight vector #1, transmit power #3, weight vector #4 }. SNR #311 and SNR #411 are calculated when the second RRU transmits the calibration reference signal to the first RRU with transmit power #3, weight vector #3, and transmit power #3, weight vector #4, respectively.

Case two:

and traversing each weight vector of the RRU receiving the correction reference signal to calculate the signal-to-noise ratio of different correction reference signals. The obtained signal-to-noise ratios respectively correspond to different subsets and are used for judging whether the corresponding subsets are selectable subset subsets.

For example, the SNR #311 and the SNR #411 may be calculated by traversing the weight vector #3 and the weight vector #4 after the third antenna and the fourth antenna in the second RRU receive the first correction reference signal sent by the first RRU with the transmission power #1 and the weight vector # 1. That is, the snr of the combined calibration reference signal does not need to be calculated for the subsets { transmit power #1, weight vector #1, transmit power #3, weight vector #3}, { transmit power #1, weight vector #1, transmit power #3, weight vector #4}, { transmit power #1, weight vector #1, transmit power #4, weight vector #3}, and { transmit power #1, weight vector #1, transmit power #4, weight vector #4}, respectively.

In summary, the measurement mode for determining the 6 measurement values of the selectable set subset may be to sequentially measure the measurement value corresponding to each subset, or may be to traverse the weight vector of the receiver after receiving the calibration reference signal for some time to calculate the signal-to-noise ratio corresponding to each of the plurality of subsets.

Assume in this particular example that the resulting subset of selectable sets includes the following four:

{ transmit power #1, weight vector #1, transmit power #3, weight vector #3}, { transmit power #1, weight vector #2, transmit power #3, weight vector #4}, { transmit power #2, weight vector #1, transmit power #4, weight vector #3}, and { transmit power #2, weight vector #2, transmit power #4, weight vector #4 }. Determining the first subset of selectable sets from the 4 subsets of selectable sets comprises the following two steps:

the method comprises the following steps: the minimum value of the two signal-to-noise ratios corresponding to the 4 subsets of the selectable sets is determined.

For example, the SNR #311 is 1, and the SNR #133 is 2; SNR # 412-3, SNR # 234-4; SNR # 331-5, SNR # 143-6; SNR #422 is 7 and SNR #244 is 8. Then determining the minimum value of the two corresponding signal-to-noise ratios from the 4 subsets of the selectable sets comprises: 1. 3, 5 and 7.

Step two: and selecting the selectable set subset corresponding to the maximum value from the minimum values as the first selectable set subset.

For example, the subset of the selectable set corresponding to "7" is determined from 1, 3, 5, and 7 to be { transmit power #2, weight vector #2, transmit power #4, weight vector #4 }. Then, the first subset of the selectable sets is { transmit power #2, weight vector #2, transmit power #4, weight vector #4 }.

It should be understood that, when the maximum value of the minimum values includes a plurality of values, one selectable set subset corresponding to one maximum value may be arbitrarily selected from the plurality of maximum values as the first selectable set subset. And will not be described in detail herein.

For example, after the plurality of selectable set subsets are determined, one selectable set subset may be determined from any of the plurality of selectable set subsets as the first selectable set subset without going through the above-mentioned step one and step two.

It should be understood that fig. 6 only illustrates how the first RRU determines the alternative set by way of example. In the actual processing process, the execution subject determining the selectable set may be the second RRU or a BBU connected to the first RRU or a BBU connected to the second RRU or other management devices, which is not limited in this application. Only the first transmit power and the first weight vector in the finally calculated subset of the selectable set need to be notified to the first RRU, and the second transmit power and the second weight vector need to be notified to the second RRU, regardless of which device the execution subject is.

The flow of the method for channel correction provided in this embodiment is described in detail above with reference to fig. 5 and fig. 6, where when determining the first transmit power, the first weight vector, the second transmit power, and the second weight vector, all elements in the first transmit power set, the first weight vector set, the second transmit power set, and the second weight vector set may be traversed to obtain the above-mentioned subset of the selectable sets including the first transmit power, the first weight vector, the second transmit power, and the second weight vector.

In practical applications, the above selectable set subset may be obtained without traversing all elements. In practical applications, how another method for channel correction provided by the embodiment of the present application is applied is described in detail below with reference to fig. 7 to 9, where the method may obtain the above-mentioned selectable set subset without traversing all elements.

Fig. 7 is a flowchart of an application of the method for channel calibration according to the embodiment of the present application. The method is applied to the correction of the receiving and transmitting channels between N RRUs, and how to correct the receiving and transmitting channels between the RRUs between any two RRUs in the N RRUs is described by taking RRUi and RRUj as examples, wherein i and j are serial numbers of different RRUs in the N RRUs, and j is not equal to i.

It should be understood that the first set of transmit powers and the first set of weight vectors described above are included in the RRUi; the RRUj includes the second set of transmit powers and the second set of weight vectors.

S310, determining a first transmitting power, a first weight vector, a second transmitting power and a second weight vector.

Specifically, S310 includes the following three stages. The three stages can be understood as a specific implementation of S230 and S240 in the method flow shown in fig. 6, where fig. 6 simply describes what conditions can be satisfied for a potential selectable set subset, and the three stages in S310 describe in detail how, in an actual application flow, 2 transmit powers and 2 weight vectors are selected from the first set of transmit powers, the first set of weight vectors, the second set of transmit powers, and the second set of weight vectors to form the potential selectable set subset, and further determine whether the formed potential selectable set subset satisfies the conditions that can be used as the selectable set subset. A first subset of the selectable sets is determined from the plurality of subsets of the selectable sets when present.

The first stage is as follows: s311, a unique selectable set subset is obtained in a mode of default transmitting power and a preset weight vector.

And the antenna in the RRUi sends the correction reference signal to the antenna in the RRUj by using the first preset transmitting power and the first preset weight vector. Wherein, the weight multiplied by the transmitted correction reference signal on the kth antenna in the RRUi is the kth element in the first preset weight vector. By default, the first preset weight vector is a unit vector with the 0 th element being 1 and the rest elements being 0 in the first weight vector set; the first preset transmission power is the minimum transmission power in the first transmission power set.

For the antenna in the RRUi to send the calibration reference signal to the antenna in the RRUj with the first preset transmit power and the first preset weight vector, the power of the calibration reference signal received on the antenna i in the RRUj is recorded as: RSRP_i00,jl(ii) a RRUj combines the correction reference signals received on all antennas into a path of correction reference signal by a second preset weight vector, and the signal-to-noise ratio of the path of correction reference signal is recorded as SNR_i00,j0And the weight on the first antenna is the first element in the second preset weight vector. By default, the second predetermined weight vector represents a unit vector in which the 0 th element is 1 and the remaining elements are 0.

And the antenna in the RRUj sends the correction reference signal to the antenna in the RRUi by using the second preset transmitting power and the second preset weight vector. Wherein, the weight multiplied by the transmitted calibration reference signal on the l antenna in the RRUj is the l element in the first preset weight vector. By default, the second preset transmit power is the smallest transmit power in the second set of transmit powers.

For the antenna in the RRUj to send the calibration reference signal to the antenna in the RRUi with the second preset transmit power and the second preset weight vector, the power of the calibration reference signal received on the antenna k in the RRUi is recorded as: RSRP_j00，ik(ii) a The RRUi combines the correction reference signals received on all the antennas into a path of correction reference signal by a first preset weight vector, and the signal-to-noise ratio of the path of correction reference signal is recorded as SNR_j00，i0And the weight on the kth antenna is the kth element in the first preset weight vector.

If RSRP_i00，jl＜Th_Upper，RSRP_j00，ik＜Th_Upper，SNR_i00，j0＞Th_Lower，SNR_j00，i0＞Th_LowerIf the four equations are satisfied, the first transmit power is the first predetermined transmit power, the first weight vector is the first predetermined weight vector, the second transmit power is the second predetermined transmit power, and the second weight vector is the second predetermined weight vector, where Th is the second predetermined weight vector_UpperIndicating an upper limit of the received power of the corrected reference signal, e.g. Th_UpperStarting and controlling threshold for receiving end AAGC), Th_LowerLower limit value representing the signal-to-noise ratio of the received correction reference signal, l ═ b_j，k＝a_iGo to S320; otherwise, the second phase is entered.

It should be understood that if it is determined in the first stage that the subset of alternatives consists of the first transmit power, the first weight vector, the second transmit power, and the second weight vector, it is equivalent to antenna 0 in RRUi sending the calibration reference signal to antenna 0 in RRUj at the default transmit power, and antenna 0 in RRUj sending the calibration reference signal to antenna 0 in RRUi at the default transmit power.

And a second stage: and S312, acquiring the unique selectable set subset in a mode of traversing the transmitting power and traversing the weight vector.

Antenna in RRUi with power P_im＝P_i，min+ Δ mdBm and weight vector w_ibThe corrected reference signal is sent to the antennas in RRUj. Wherein, the weight value multiplied by the transmitted correction reference signal on the k antenna in RRUi is w_ibWherein m is 0,1_i-1，b＝1，2，...，B_i，L_iIs the number of transmission powers in the first set of transmission powers, B_iThe number of weight vectors, P, traversed by RRUi in the second stage_i，minFor the first preset transmit power in the first phase, Δ is default to 10. In the second stage, the L is traversed by adopting a mode of randomly combining time division, frequency division (combing) and code division_iA transmission power value and B_iA weight vector. Typically, first, traverse B with the 0 th transmit power value_iA weight vector is then used1 st transmission power value traversal B_iA weight vector, analogizing, and so on; the traversal of different transmitting power values can be completed in a time division mode, and the traversal of different weight vectors can be completed in a time division, frequency division (combing) or code division mode.

Illustratively, the weight vector w_ibThe design of (2) may use a vector with partial or total element value of 1, a vector based on Discrete Fourier Transform (DFT), or a combination of the two. A vector having a partial or total element value of 1 means w_ibA vector in which some or all of the elements of (1) are 1 and the remaining elements are 0.

For example, w_ibDenotes the former b.DELTA._bVector with 1 for each element and 0 for the remaining elements, default Δ_b8. The vector based on discrete Fourier transform refers to w_ibGenerated by a DFT sequence, the DFT sequence with beam number p and length K (row vector) can be represented as w_DFT(p，K)，w_DFTThe kth element of (p, K) isj represents an imaginary unit, K is 0, 1. The RRUi antenna is assumed to be in a dual-polarized and horizontal direction K_horizontalIndividual subarrays, vertical direction K_verticalArray of sub-arrays, total 2K_horizontalK_verticalAnd (5) sub-arrays. Numbering the antennas horizontally, vertically and finally in polarization mode

Where pib denotes the traversal beam number in the vertical direction, qib denotes the traversal beam number in the horizontal direction, and the symbolRepresenting the Kronecker (Kronecker) product of the matrix. For vectors using discrete Fourier transform based, one traversal beam number pair P_ibAnd q is_ibUniquely determine a weight directionAmount, typically, p_ibIs a fixed value (default p)_ib＝0)，q_ib＝bΔ_b(Default. DELTA.)_b＝4)。

For the antenna in RRUi to send the calibration reference signal to the antenna in RRUj with the mth transmission power value and the mth weight vector, the power of the calibration reference signal received on the antenna i in RRUj is expressed as: RSRP_imb，jlRRUj bases the corrected reference signals received on all antennas on weight vector w_jdCombining into a correction reference signal, and recording the signal-to-noise ratio of the correction reference signal as SNR_imb，jdWherein the weight on the first antenna is w_jdThe ith element of (1). Weight vector w_jdDesign of (2) and the above-mentioned w_ibThe design of (2) is consistent, a vector with partial or whole element values of l can be adopted, a vector based on discrete Fourier transform can be adopted, or a combination of the two.

It should be appreciated that the RRUj described above bases the corrected reference signals received on all antennas on the weight vector w_jdThe combination into a path of corrected reference signal is only for convenience of the subsequent RRUj based on the weight vector w_jdAn example of the description of sending the calibration reference signal cannot illustrate that when the antenna in the RRUi sends the calibration reference signal to the antenna in the RRUj with the mth transmission power value and the mth weight vector, the RRUj can only send the calibration reference signal received by all antennas with the weight vector w_jdThe signals are combined into a path of calibration reference signal, and it should be understood that RRUj can traverse each weight vector in RRUj with the calibration reference signals received on all antennas, and combine each weight vector to obtain multiple paths of calibration reference signals, and calculate the signal-to-noise ratio of each path of calibration reference signal in the multiple paths of calibration reference signals.

Antenna in RRUj with power P_jn＝P_j，min+ Δ ndBm and weight vector w_jdThe corrected reference signal is sent to the antennas in the RRUi. Wherein, the weight value multiplied by the correction reference signal transmitted on the l antenna in RRUj is w_jdThe first element in (1), n is 0,1_j-1，d＝1，1，...，B_j，L_jIs the number of transmission powers in the second set of transmission powers, B_jThe number of weight vectors, P, traversed by RRUj in the second stage_j，minFor the second preset transmit power in the first phase, Δ is default to 10. In the second stage, the B is traversed by adopting a mode of randomly combining time division, frequency division (combing) and code division_jA weight vector.

For the antenna in RRUj to send the calibration reference signal to the antenna in RRUi with the nth transmit power value and the d weight vector, the power of the calibration reference signal received on the antenna k in RRUi is expressed as: RSRP_jnd，ikRRUi bases the corrected reference signals received on all antennas on the weight vector w_ibCombining into a correction reference signal, and recording the signal-to-noise ratio of the correction reference signal as SNR_jnd，ibWherein the weight on the kth antenna is w_ibThe kth element of (1).

It should be understood that the RRUi described above bases the corrected reference signals received on all antennas on the weight vector w_ibCombining into a path of calibration reference signal is only an example, and it cannot be said that when an antenna in an RRUi sends a calibration reference signal to an antenna in the RRUi by using an nth transmission power value and a d weight vector, the RRUi can only send the calibration reference signal received on all antennas by using the weight vector w_ibThe signals are combined into a path of calibration reference signal, and it should be understood that the RRUi may traverse each weight vector in the RRUi with the calibration reference signals received on all antennas, combine each weight vector to obtain multiple paths of calibration reference signals, and calculate the signal-to-noise ratio of each path of calibration reference signal in the multiple paths of calibration reference signals.

Satisfying RSRP_imb，jl＜Th_Upper，RSRP_jnd，ik＜Th_Upper，SNR_imb，jd＞Th_Lower，SNR_jnd，ib＞Th_LowerFour equations of transmit power and weight vector { P }_im，w_ib，P_jn，w_jdForm an optional set C_imb，jndWherein, Th_UpperAnd Th_LowerHas the same meaning as in the first stage, l is w_jdThe number of the middle element being nonzero, k being w_ibThe non-zero sequence number of the middle element. If no optional subset exists, entering a third stage; if optional set existsA subset selected from all selectable sets such that SNR_imb，jdAnd SNR_jnd，ibThe subset of the selectable set with the maximum minimum value (if there are multiple same maximum values, one is selected) is recorded as

Is expressed asThe first transmit power, the first weight vector, the second transmit power, and the second weight vector are a subset of the selectable setThe process proceeds to S320.

And a third stage: and S313, acquiring the unique selectable set subset in a mode of default transmitting power and traversing weight vectors.

Antenna in RRUi with power P_i0＝P_i，mindBm and weight vector v_ibThe corrected reference signal is sent to the antennas in RRUj. Wherein, the weight value multiplied by the transmitted correction reference signal on the k antenna in the RRUi is v_ibThe k-th element of (a), wherein,

the number of weight vectors, P, traversed by RRUi in the third stage_i，minIs the first preset transmitting power in the first stage.

Illustratively, the weight vector v_ibThe design of (2) may be: v. of_ibF of (a)_iThe value of each element is

v_ibG of (2)_iThe value of each element is

All other elements have a value of 0, wherein_iRoot antenna and g_iThe root antenna is two antennas which are most adjacent in the horizontal direction of the same polarization on the RRUi.

For the 0 th transmission power value and the b th weight vector of the RRUi to send the calibration reference signal to the antenna in the RRUj, the power of the calibration reference signal received on the antenna i in the RRUj is recorded as: RSRP_i0b，jlRRUj bases the corrected reference signals received on all antennas on the weight vector v_jdCombining into a correction reference signal, and recording the signal-to-noise ratio of the correction reference signal as SNR_i0b，jdWherein the weight value on the l antenna is v_jdThe first element of (a), v_jdDesign of (c) and (v)_ibAnd (5) the consistency is achieved.

Antenna in RRUj with power P_j0＝P_j，mindBm and weight vector v_jdThe corrected reference signal is sent to the antennas in the RRUi. Wherein, the weight value multiplied by the correction reference signal transmitted on the l antenna in RRUj is v_jdThe first element of (a), wherein,

the number of weight vectors, P, traversed by RRUj in the third stage_j，minIs the second preset transmitting power in the first stage.

For the 0 th transmission power value and the d weight vector of RRUj, the power of the corrected reference signal received on the antenna k of RRUi is marked as RSRP_j0d，ikAnd the corrected reference signals received on all antennas are based on the weight vector w_ib＝v_ibCombining into a correction reference signal, and recording the signal-to-noise ratio of the correction reference signal as SNR_j0d，ibWherein the weight value on the k antenna is v_ibThe kth element of (1).

Satisfying RSRP_i0b，jl＜Th_Upper，RSRP_j0d，ik＜Th_Upper，SNR_i0b，jd＞Th_Lower，SNR_j0d，ib＞Th_LowerWeight vector of four equations v_ib，v_jdStructure ofTo form a selectable set C_ib，jdWherein, Th_UpperAnd Th_LowerHas the same meaning as in the first stage, l is w_jdThe number of the middle element being nonzero, k being w_ibThe non-zero sequence number of the middle element. If no optional set subset exists, RRUi and RRUj are not communicated and cannot be corrected; if there are subsets of the alternative sets, all of the alternative sets are selected such that the SNR is equal to_i0b，jdAnd SNR_j0d，ibThe subset of the selectable set with the maximum minimum value (if there are multiple same maximum values, one is selected) is recorded asThe first transmit power, the first weight vector, the second transmit power and the second weight vector are

Is expressed asWhere min { a, b } represents the smaller of the numbers a and b, and arqmax { A } represents the subset of the alternative set that maximizes the value of expression A in parentheses.

And S320, calculating a correction coefficient.

For convenience of description, the first predetermined transmission power is referred to asThe first predetermined weight vector isA second predetermined transmission power ofThe second predetermined weight vector is

Antenna in RRUi with powerAnd weight vector

The corrected reference signal is sent to the antennas in RRUj. Wherein, the weight value multiplied by the transmitted correction reference signal on the k antenna in RRUi isThe k-th element in (2), all antennas in RRUj receive the corrected reference signal and base all received corrected reference signals on weight vectors

The signals are combined into a path of corrected reference signal (signal #1), and the weight value on the first antenna of RRUj is

The ith element of (1).

Antenna in RRUj with powerAnd weight vectorThe corrected reference signal is sent to the antennas in the RRUi. Wherein, the weight value multiplied by the correction reference signal transmitted on the l antenna in RRUj isAll antennas of the RRUi receive the calibration reference signal and base all received calibration reference signals on weight vectors

The signals are combined into a path of correction reference signal (signal #2), and the weight value on the k antenna of RRUi is

The kth element of (1).

Finally, a correction coefficient is calculated based on the signal #1 and the signal # 2.

In the application flow shown in fig. 7, in the first phase, the calibration reference signal is received and transmitted by using the lowest transmission power and a single antenna, and whether the calibration requirement is met is tried to be met; in the second stage, the transmitting power and the weight vector are traversed simultaneously, and the design of the weight vector is to improve the power of the received correction reference signal; in the second stage, the lowest transmission power is adopted, that is, the transmission power is not traversed, and only the weight vector is traversed, and the design of the weight vector is to reduce the power of the received calibration reference signal. In the application flow shown in fig. 7, two-dimensional traversal of the transmission power and the weight vector is performed, so that the dynamic range of the received power of the calibration reference signal is significantly expanded, and the appropriate received power of the calibration reference signal can be obtained. The embodiment is suitable for a multi-cell channel correction scene with mixed co-station and non-co-station, and can solve the problem that the correction cannot be performed due to overhigh or overlow correction reference signal power.

Compared with the technical solution of the embodiment of fig. 3, the application process shown in fig. 7 can raise or lower the power of the received calibration reference signal by the weight vector, so as to solve the problem that the power of the calibration reference signal is too low or too high to be calibrated. Compared with the technical solution of the embodiment of fig. 4, the application process shown in fig. 7 can reduce the power of the received calibration reference signal through the weight vector, and solve the problem of overhigh power of the calibration reference signal; the two RRUs both adopt weights, and higher received corrected reference signal power can be provided; and the time overhead required for dynamically calculating the dynamic weight can be saved by adopting the weight.

Fig. 8 is a flowchart of another application of the method for channel correction according to the embodiment of the present application. The method is applied to the correction of the transceiving channel between N RRUs, and is described by taking RRUi and RRUj as examples, wherein i and j are the serial numbers of different RRUs in the N RRUs, and j is not equal to i.

It should be understood that the first set of transmit powers and the first set of weight vectors described above are included in the RRUi; the RRUj includes the second set of transmit powers and the second set of weight vectors.

S410, determining a first transmitting power, a first weight vector, a second transmitting power and a second weight vector.

Specifically, S410 includes the following two stages.

The first stage is as follows: s411, a unique selectable set subset is obtained in a mode of traversing the transmitting power and the preset weight vector.

Antenna in RRUi with power P_im＝P_i，minThe + Δ · mdBm and the first preset weight vector send a calibration reference signal to the antennas in RRUj. Wherein, the weight multiplied by the transmitted correction reference signal on the kth antenna in the RRUi is the kth element in the first preset weight vector. Wherein, m is 0,1_i-1，L_iThe default delta is 10 for the number of the transmission power in the first transmission power set; the first preset weight vector is a unit vector in which the 0 th element in the first weight vector set is 1 and the rest elements are 0.

For antenna in RRUi with power P_im＝P_i，minFor + Δ · mdBm and the first preset weight vector to send the calibration reference signal to the antenna in RRUj, the power of the calibration reference signal received on the antenna l in RRUj is recorded as: RSRP_im0，jl(ii) a RRUj combines the correction reference signals received on all antennas into a path of correction reference signal by a second preset weight vector, and the signal-to-noise ratio of the path of correction reference signal is recorded as SNR_im0，j0And the weight on the first antenna is the first element in the second preset weight vector. By default, the second predetermined weight vector represents a unit vector in which the 0 th element is 1 and the remaining elements are 0.

Antenna in RRUj with power P_jn＝P_j，minAnd the + delta ndBm and the second preset weight vector send a correction reference signal to an antenna in the RRUi. Wherein, the weight multiplied by the transmitted calibration reference signal on the L antenna in the RRUj is the L element in the first preset weight vector, n is 0,1_j-1，L_jThe number of the transmission powers in the second transmission power set. By default, Δ ═ 10.

With power P for antennas in RRUj_jn＝P_j，minTo the extent that + Δ. ndBm and the second predetermined weight vector send the calibration reference signal to the antennas in RRUi,the power of the corrected reference signal received on antenna k in RRUi is noted as: RSRP_jn0，ik(ii) a The RRUi combines the correction reference signals received on all the antennas into a path of correction reference signal by a first preset weight vector, and the signal-to-noise ratio of the path of correction reference signal is recorded as SNR_jn0，i0And the weight on the kth antenna is the kth element in the first preset weight vector.

Satisfying RSRP_im0，jl＜Th_Upper，RSRP_jn0，ik＜Th_Upper，SNR_im0，j0＞Th_Lower，SNR_jn0，i0＞Th_LowerFour equation transmit powers P_im，P_jnForm an optional set G_im，jnWherein, Th_UpperIndicating an upper limit value, Th, of the received corrected reference signal power_LowerLower limit value representing the signal-to-noise ratio of the received correction reference signal, l ═ b_j，k＝a_i. If no optional set subset exists, entering a second stage; if there are subsets of the alternative sets, all of the subsets of the alternative sets are selected such that the SNR is greater than the threshold_im0，j0And SNR_jn0，i0The subset of the selectable set with the maximum minimum value (if there are multiple same maximum values, one is selected) is recorded asIs expressed as

The first transmit power, the first weight vector, the second transmit power and the second weight vector areA first predetermined weight vector is set to be a first predetermined weight vector,

a second preset weight vector }, and then the process goes to S420; otherwise, the second phase is entered.

And a second stage: and S412, acquiring the unique selectable set subset in a mode of traversing the transmitting power and traversing the weight vector.

In RRUiAt power ofAnd weight vector w_ibThe corrected reference signal is sent to the antennas in RRUj. Wherein, the weight value multiplied by the transmitted correction reference signal on the k antenna in RRUi is w_ibOf (b), wherein m is^*＝L_i-1，b＝1，2，...，B_i，L_iIs the number of transmission powers in the first set of transmission powers, B_iThe number of the weight vectors in the second weight vector set is shown. In the second stage, the B is traversed by adopting a mode of randomly combining time division, frequency division (combing) and code division_iA weight vector. Weight vector w_ibLike the second stage shown in fig. 6, it will not be described again here.

For the antenna in RRUi by m^*For the case that the transmission power value and the b-th weight vector send the calibration reference signal to the antenna in RRUj, the power of the calibration reference signal received by the antenna l in RRUj is recorded as:RRUj bases the correction reference signals received on all antennas on weight vector w_jdCombining the signals into a corrected reference signal, and recording the signal-to-noise ratio of the corrected reference signal as

Wherein, the weight on the first antenna is w_jdThe ith element of (1). Weight vector w_jdDesign of (2) and the above-mentioned w_ibThe design of (2) is consistent, a vector with partial or all element values of 1 can be adopted, a vector based on discrete Fourier transform can be adopted, or a combination of the two.

Antenna in RRUj with powerAnd weight vector w_jdThe corrected reference signal is sent to the antennas in the RRUi. Wherein, the weight value multiplied by the correction reference signal transmitted on the l antenna in RRUj is w_jdThe 1 st element, n^*＝L_j-1，d＝1，1，...，B_j，B_jThe number of the weight vectors in the second weight vector set is shown.

For the antenna in RRUj with the nth^*For the reason that the transmission power value and the d-th weight vector send the calibration reference signal to the antenna in the RRUi, the power of the calibration reference signal received on the antenna k in the RRUi is recorded as:RRUi bases the correction reference signals received on all antennas on weight vector w_ibCombining the signals into a corrected reference signal, and recording the signal-to-noise ratio of the corrected reference signal as

Wherein, the weight value on the k antenna is w_ibThe kth element of (1).

Satisfy the requirement of Four equations of transmit power and weight vector w_ib，w_jdForm an optional set C_ib，jdWherein, Th_UpperAnd Th_LowerHas the same meaning as in the first stage, l is w_jdThe number of the middle element being nonzero, k being w_ibThe non-zero sequence number of the middle element. If no optional set subset exists, RRUi and RRUj are not communicated and cannot be corrected; if there are subsets of the alternative sets, all of the subsets of the alternative sets are selected such that

And

the subset of the selectable set corresponding to the maximum value of the two minimum values (if there are multiple same maximum values, one is selected) is recorded as

Is expressed as

The first transmit power, the first weight vector, the second transmit power and the second weight vector are

The process proceeds to S420.

And S420, calculating a correction coefficient.

Similar to S320 shown in fig. 7, will not be described again here.

The main differences between the application flow shown in fig. 8 and the application flow shown in fig. 7 are that:

in the process of determining the first transmit power, the first weight vector, the second transmit power and the second weight vector, the purpose of the weight vector is to increase the power of the received calibration reference signal without reducing the power of the received calibration reference signal, and the method is mainly suitable for a calibration scenario of a transmit-receive channel between non-co-station multiple RRUs.

The application flow shown in fig. 8 divides the two-dimensional traversal problem of the transmission power and the weight vector into two one-dimensional traversal problems in a time division manner: in the first stage, two RRUs adopt a single antenna to receive and transmit correction reference signals, namely, a weight vector is not traversed, and only transmission power is traversed; in the second stage, the two RRUs both use the maximum transmission power, that is, the transmission power is not traversed, and only the weight vector is traversed. In the first stage, whether the traditional single-antenna scheme is adopted can be judged to meet the correction requirement, and if the traditional single-antenna scheme is not adopted, the power of the received correction reference signal is obviously improved through the transmitting/receiving weight value vector in the second stage. The application flow shown in fig. 8 is particularly suitable for a transceiver channel correction scenario among multiple non-co-located RRUs, and can solve the problem that the correction cannot be performed due to too low power of the correction reference signal.

Compared with the technical solution of the embodiment of fig. 3, the application process shown in fig. 8 can significantly improve the power of the received calibration reference signal through the weight vector, and solve the problem that the calibration reference signal power is too low to cause calibration failure. Compared with the technical solution of the embodiment of fig. 4, the application flow shown in fig. 8 has two RRUs both using weights, which can provide higher received power of the calibration reference signal; and the time overhead and the overhead required by dynamically calculating the dynamic weight can be saved by adopting the weight: the weight can be designed into a wide beam, frequent traversal is not needed, and time and expense are saved; the weight value does not need to be calculated, so that the calculation cost is avoided.

Fig. 9 is a flowchart of another application of the method for channel correction according to the embodiment of the present application. The method is applied to the correction of the transceiving channel between N RRUs, and is described by taking RRUi and RRUj as examples, wherein i and j are the serial numbers of different RRUs in the N RRUs, and j is not equal to i.

It should be understood that the first set of transmit powers and the first set of weight vectors described above are included in the RRUi; the RRUj includes the second set of transmit powers and the second set of weight vectors.

S510, determining a first transmitting power, a first weight vector, a second transmitting power and a second weight vector.

Specifically, S510 includes the following two stages.

The first stage is as follows: and S511, acquiring the unique selectable set subset in a mode of default transmitting power and a preset weight vector.

Similar to S311 shown in fig. 7, no further description is provided here.

And a second stage: s512, acquiring the unique selectable set subset in a mode of default transmitting power and traversal weight vector.

Antenna in RRUi with power P_i0＝P_i，mindBm and weight vector v_ibThe corrected reference signal is sent to the antennas in RRUj. Wherein, the weight value multiplied by the transmitted correction reference signal on the k antenna in the RRUi is v_ibWherein, B is 1, 2_i，B_iIs the number of weight vectors in the first weight vector set, P_i，minIs the first preset transmitting power in the first stage.

Illustratively, the weight vector v_ibAnd the design weight vector v referred to in S313 shown in fig. 6_ibSimilarly, no further description is provided herein.

For the 0 th transmission power value and the b th weight vector of the RRUi to send the calibration reference signal to the antenna in the RRUj, the power of the calibration reference signal received on the antenna i in the RRUj is recorded as: RSRP_i0b，jlRRUj bases the corrected reference signals received on all antennas on the weight vector v_jdCombining into a correction reference signal, and recording the signal-to-noise ratio of the correction reference signal as SNR_i0b，jdWherein the weight value on the l antenna is v_jdThe first element of (a), v_jdDesign of (c) and (v)_ibAnd (5) the consistency is achieved.

Antenna in RRUj with power P_j0＝P_j，mindBm and weight vector v_jdThe corrected reference signal is sent to the antennas in the RRUi. Wherein, the weight value multiplied by the correction reference signal transmitted on the l antenna in RRUj is v_jdWherein, d is 1, 1_j，B_jIs the number of weight vectors in the second weight vector set, P_j，minIs the second preset transmitting power in the first stage.

For the 0 th transmission power value and the d weight vector of RRUj, the power of the corrected reference signal received on the antenna k of RRUi is marked as RSRP_j0d，ikAnd the corrected reference signals received on all antennas are based on the weight vector w_ib＝v_ibCombining into a correction reference signal, and recording the signal-to-noise ratio of the correction reference signal as SNR_j0d，ibWherein the weight value on the k antenna is v_ibThe kth element of (1).

Satisfying RSRP_i0b，jl＜Th_Upper，RSRP_j0d，ik＜Th_Upper，SNR_i0b，jd＞Th_Lower，SNR_j0d，ib＞Th_LowerWeight vector of four equations v_ib，v_jdForm an optional set C_ib，jdWherein, Th_UpperAnd Th_LowerHas the same meaning as in the first stage, l is w_jdThe number of the middle element being nonzero, k being w_ibThe non-zero sequence number of the middle element. If no optional set subset exists, RRUi and RRUj are not communicated and cannot be corrected; if there is a subset of the alternative sets, from all alternative setsThe sub-set is selected such that the SNR_i0b，jdAnd SNR_j0d，ibThe subset of the selectable sets (one of which is optional if there are multiple same maximum values) corresponding to the maximum value of the two minimum values is recorded asIs expressed asThe first transmit power, the first weight vector, the second transmit power and the second weight vector areWhere min { a, b } represents the smaller of the numbers a and b, and argmax { a } represents the subset of the selectable set that maximizes the value of expression a in parentheses, and the process proceeds to S520.

And S520, calculating a correction coefficient.

Similar to S320 shown in fig. 7, will not be described again here.

The main difference between the application flow shown in fig. 9 and the application flow shown in fig. 7 is that:

in the process of determining the first transmit power, the first weight vector, the second transmit power and the second weight vector, the purpose of the weight vector is to reduce the power of the received calibration reference signal without improving the received power of the calibration reference signal, and the method is mainly suitable for a calibration scenario of a transmit-receive channel among multiple RRUs in a common station.

The application flow shown in fig. 9 divides the two-dimensional traversal problem of the transmission power and the weight vector into two one-dimensional traversal problems in a time division manner: in the first stage, two RRUs adopt a single antenna to receive and transmit correction reference signals, namely, a weight vector is not traversed, and only transmission power is traversed; in the second stage, the two RRUs both use the lowest transmit power, that is, the transmit power is not traversed, and only the weight vector is traversed. In the first stage, whether the traditional single-antenna scheme is adopted can be judged to meet the correction requirement, and if the traditional single-antenna scheme is not adopted, the power of the received correction reference signal is reduced through the transmitting/receiving weight value vector in the second stage. The application flow shown in fig. 9 is particularly suitable for a transceiver channel calibration scenario among multiple RRUs sharing a station, and can solve the problem that the calibration cannot be performed due to too high power of the calibration reference signal.

Compared with the technical solution of the embodiment of fig. 3, the application process shown in fig. 9 can significantly improve the power of the received calibration reference signal through the weight vector, and solve the problem that the calibration reference signal cannot be corrected due to too high power. Compared with the technical solution of the embodiment of fig. 4, the application flow shown in fig. 9 can reduce the received power of the calibration reference signal; and the time overhead required for dynamically calculating the dynamic weight can be saved by adopting the weight.

It should be understood that, in each method embodiment, the sequence numbers of the processes do not mean the execution sequence, and the execution sequence of each process should be determined by the function and the inherent logic of the process, and should not constitute any limitation to the implementation process of the embodiment of the present application.

The method for channel correction provided by the embodiment of the present application and the specific application flow of the method for channel correction are described in detail above with reference to fig. 5 to 9. The first RRU and the second RRU provided in the present application are described in detail below with reference to fig. 10 to fig. 13.

Fig. 10 is a schematic diagram of a first RRU10 according to an embodiment of the present application. As shown in fig. 10, the first RRU10 includes a sending unit 110, a receiving unit 120, and a processing unit 130.

A sending unit 110, configured to send a first calibration reference signal to the third antenna and the fourth antenna through the first antenna and with a first transmit power and a first weight vector;

the sending unit 110 is further configured to send, through the second antenna, a second correction reference signal to the third antenna and the fourth antenna by using the first transmit power and the first weight vector, where the first transmit power is a transmit power in a preset first transmit power set, and the first weight vector is a weight vector in a preset first weight vector set.

A receiving unit 120, configured to receive, through the first antenna and the second antenna, third calibration reference signals that are respectively sent by the second RRU through the third antenna with a second transmission power and a second weight vector;

the receiving unit 120 is further configured to receive, through the first antenna and the second antenna, a fourth calibration reference signal that is sent by the second RRU through the fourth antenna with a second transmit power and a second weight vector, where the second transmit power is one transmit power in a preset second transmit power set, and the second weight vector is one weight vector in a preset second weight vector set.

A processing unit 130, configured to combine the calibration reference signals received at the first antenna and the second antenna into a sixth calibration reference signal, and combine the calibration reference signal received at the third antenna and the calibration reference signal received at the fourth antenna into a fifth calibration reference signal. And the fifth correction reference signal and the sixth correction reference signal are used for calculating a correction coefficient of a transceiving channel between the first RRU and the second RRU.

The first RRU10 corresponds exactly to the first RRU in the method embodiment, and the corresponding units of the first RRU10 are used to perform the corresponding steps performed by the first RRU in the method embodiments shown in fig. 5-9.

Wherein, the sending unit 110 in the second RRU10 performs the step of sending by the first RRU in the method embodiment. For example, step 110 of fig. 5 of sending the first and second corrected reference signals to the second RRU is performed. The receiving unit 120 performs the step of receiving by the first RRU in the method embodiment. For example, step 130 of fig. 5 receiving the third and fourth corrected reference signals is performed. The processing unit 130 performs the steps implemented or processed inside the first RRU in the method embodiment. For example, step 140 of fig. 5 of acquiring a sixth corrected reference signal is performed.

Alternatively, the receiving unit 120 and the transmitting unit 110 may constitute a transceiving unit, and have both receiving and transmitting functions. Wherein the processing unit 130 may be a processor. The transmitting unit 110 may be a receiver. The receiving unit 120 may be a transmitter. The receiver and transmitter may be integrated together to form a transceiver.

Referring to fig. 11, fig. 11 is a schematic structural diagram of an apparatus for channel correction suitable for the embodiment of the present application, which can be used to implement the function of the first RRU in the method for channel correction described above. For example, the apparatus may be the first RRU described above, or the apparatus may be a chip inside the first RRU, which is capable of implementing the method for channel correction described above, or other devices capable of implementing the function of the first RRU in the method for channel correction described above. In particular, the apparatus may include a processor 210 (i.e., an example of the processing unit 120 in fig. 10) and a memory 220. The memory 220 is used to store instructions.

The processor 210 is configured to execute the instructions stored in the memory 220 to enable the apparatus to implement the steps performed by the first RRU in the method described above.

Further, the apparatus may further include an input port 230 and an output port 240 (i.e., an example of the receiving unit and the transmitting unit 110 of fig. 10). Further, the processor 210, memory 220, input port 230, and output port 240 may communicate with each other via internal communication paths to communicate control and/or data information. The memory 220 is used for storing a computer program, and the processor 210 may be used for calling and running the computer program from the memory 220 to control the input port 230 to receive information and the output port 240 to send information, so as to complete the steps of the first RRU in the above-mentioned method. The memory 220 may be integrated in the processor 210 or may be provided separately from the processor 210.

Optionally, the input port 230 is a receiver and the output port 240 is a transmitter. Wherein the receiver and the transmitter may be the same or different physical entities. When the same physical entity, may be collectively referred to as a transceiver.

Fig. 12 is a schematic diagram of a second RRU30 provided in this embodiment of the present application. As shown in fig. 12, the second RRU30 includes a sending unit 310, a receiving unit 320, and a processing unit 330.

A sending unit 310, configured to send a third calibration reference signal to the first antenna and the second antenna through the third antenna with a second transmit power and a second weight vector;

the sending unit 310 is further configured to send a fourth calibration reference signal to the first antenna and the second antenna through the fourth antenna by using a second transmit power and a second weight vector, where the second transmit power is a transmit power in a preset second transmit power set, and the second weight vector is a weight vector in a preset second weight vector set.

A receiving unit 320, configured to receive, through the third antenna and the fourth antenna, first calibration reference signals that are respectively sent by the first RRU through the first antenna with a first transmit power and a first weight vector;

the receiving unit 320 is further configured to receive, through the third antenna and the fourth antenna, second calibration reference signals that are respectively sent by the first RRU through the second antenna with a first transmit power and a first weight vector, where the first transmit power is one transmit power in a preset first transmit power set, and the first weight vector is one weight vector in a preset first weight vector set.

A processing unit 330, configured to combine the calibration reference signals received at the third antenna and the calibration reference signals received at the fourth antenna into a fifth calibration reference signal, and combine the calibration reference signal received at the first antenna and the calibration reference signal received at the second antenna into a sixth calibration reference signal; the fifth and sixth calibration reference signals are used to calculate calibration coefficients of a transceiver channel between the first RRU and the second RRU.

The second RRU30 corresponds exactly to the second RRU in the method embodiment, and the corresponding units of the second RRU30 are used to perform the corresponding steps performed by the second RRU in the method embodiments shown in fig. 5-9.

Wherein the sending unit 310 in the second RRU30 performs the steps of the second RRU sending in the method embodiment. For example, step 130 of fig. 5 of sending the third and fourth corrected reference signals to the first RRU is performed. The receiving unit 320 performs the step of receiving by the second RRU in the method embodiment. For example, step 110 of fig. 5 of receiving the first corrected reference signal and the second corrected reference signal is performed. The processing unit 330 performs the steps implemented or processed inside the second RRU in the method embodiment. For example, step 120 of fig. 5 of acquiring a fifth corrected reference signal is performed.

Alternatively, the receiving unit 320 and the transmitting unit 310 may constitute a transceiving unit, and have both receiving and transmitting functions. Wherein the processing unit 330 may be a processor. The transmitting unit 310 may be a receiver. The receiving unit 320 may be a transmitter. The receiver and transmitter may be integrated together to form a transceiver.

Referring to fig. 13, fig. 13 is a schematic structural diagram of another apparatus for channel correction suitable for this embodiment, which can be used to implement the function of the second RRU in the method for channel correction described above. For example, the apparatus may be the second RRU described above, or the apparatus may be a chip inside the second RRU, which is capable of implementing the method for channel correction described above, or other devices capable of implementing the function of the second RRU in the method for channel correction described above. In particular, the apparatus may include a processor 410 (i.e., an example of processing unit 320 in fig. 12) and a memory 420. The memory 420 is used to store instructions.

The processor 410 is configured to execute the instructions stored by the memory 420 to cause the apparatus to implement the steps performed by the second RRU in the method described above.

Further, the apparatus may further include an input port 430 and an output port 440 (i.e., an example of the sending unit 310 of the receiving unit and 320 in fig. 12). Further, the processor 410, memory 420, input port 430, and output port 440 may communicate with each other via internal communication paths to communicate control and/or data information. The memory 420 is used for storing a computer program, and the processor 410 can be used for calling and running the computer program from the memory 420 to control the input port 430 to receive information and the output port 440 to send information, so as to complete the steps of the second RRU in the above-mentioned method. The memory 420 may be integrated in the processor 410 or may be provided separately from the processor 410.

Optionally, the input port 430 is a receiver and the output port 440 is a transmitter. Wherein the receiver and the transmitter may be the same or different physical entities. When the same physical entity, may be collectively referred to as a transceiver.

An embodiment of the present application further provides a system, which includes the foregoing one or more first RRUs and second RRUs.

The present application also provides a computer-readable storage medium having stored therein instructions that, when executed on a computer, cause the computer to perform the steps performed by the first RRU in the methods described above and illustrated in fig. 5-9.

The present application also provides a computer-readable storage medium having stored therein instructions that, when executed on a computer, cause the computer to perform the steps performed by the second RRU in the methods described above and shown in fig. 5-9.

The present application also provides a computer program product comprising instructions which, when run on a computer, cause the computer to perform the steps performed by the first RRU in the method as shown in fig. 5-9.

The present application also provides a computer program product comprising instructions which, when run on a computer, cause the computer to perform the steps performed by the second RRU in the method as shown in fig. 5-9.

The application also provides a chip comprising a processor. The processor is configured to read and execute a computer program stored in the memory to perform corresponding operations and/or procedures performed by the first RRU in the method for channel correction provided in the present application. Optionally, the chip further comprises a memory, the memory is connected with the processor through a circuit or a wire, and the processor is used for reading and executing the computer program in the memory. Further optionally, the chip further comprises a communication interface, and the processor is connected to the communication interface. The communication interface is used for receiving data and/or information needing to be processed, and the processor acquires the data and/or information from the communication interface and processes the data and/or information. The communication interface may be an input output interface.

The application also provides a chip comprising a processor. The processor is configured to call and run a computer program stored in the memory to perform corresponding operations and/or procedures performed by the second RRU in the method for channel correction provided by the present application. Optionally, the chip further comprises a memory, the memory is connected with the processor through a circuit or a wire, and the processor is used for reading and executing the computer program in the memory. Further optionally, the chip further comprises a communication interface, and the processor is connected to the communication interface. The communication interface is used for receiving data and/or information needing to be processed, and the processor acquires the data and/or information from the communication interface and processes the data and/or information. The communication interface may be an input output interface.

Those of ordinary skill in the art will appreciate that the various illustrative elements and algorithm steps described in connection with the embodiments disclosed herein may be implemented as electronic hardware or combinations of computer software and electronic hardware. Whether such functionality is implemented as hardware or software depends upon the particular application and design constraints imposed on the implementation. Skilled artisans may implement the described functionality in varying ways for each particular application, but such implementation decisions should not be interpreted as causing a departure from the scope of the present application.

It is clear to those skilled in the art that, for convenience and brevity of description, the specific working processes of the above-described systems, apparatuses and units may refer to the corresponding processes in the foregoing method embodiments, and are not described herein again.

In the several embodiments provided in the present application, it should be understood that the disclosed system, apparatus and method may be implemented in other ways. For example, the above-described apparatus embodiments are merely illustrative, and for example, the division of the units is only one logical division, and other divisions may be realized in practice, for example, a plurality of units or components may be combined or integrated into another system, or some features may be omitted, or not executed. In addition, the shown or discussed mutual coupling or direct coupling or communication connection may be an indirect coupling or communication connection through some interfaces, devices or units, and may be in an electrical, mechanical or other form.

The units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the units can be selected according to actual needs to achieve the purpose of the solution of the embodiment.

In addition, functional units in the embodiments of the present application may be integrated into one processing unit, or each unit may exist alone physically, or two or more units are integrated into one unit.

The functions, if implemented in the form of software functional units and sold or used as a stand-alone product, may be stored in a computer readable storage medium. Based on such understanding, the technical solution of the present application or portions thereof that substantially contribute to the prior art may be embodied in the form of a software product stored in a storage medium and including instructions for causing a computer device (which may be a personal computer, a server, or a network device) to execute all or part of the steps of the method according to the embodiments of the present application. And the aforementioned storage medium includes: various media capable of storing program codes, such as a usb disk, a removable hard disk, a read-only memory (ROM), a Random Access Memory (RAM), a magnetic disk, or an optical disk.

The above description is only for the specific embodiments of the present application, but the scope of the present application is not limited thereto, and any person skilled in the art can easily conceive of the changes or substitutions within the technical scope of the present application, and shall be covered by the scope of the present application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.