阅读说明：本技术 一种三轴光纤陀螺精密分频方法 (Precise frequency division method for triaxial fiber-optic gyroscope ) 是由 林毅 年海涛 马骏 郑志胜 于 2019-11-21 设计创作，主要内容包括：本发明涉及一种三轴光纤陀螺精密分频方法,其特征在于：所述分频方法的步骤为：1)外部时钟基准及两级DCM设计；2)两级DCM方案时序处理；3)精密分频改进；4)分频参数算法计算。本发明设计科学合理,在不改变陀螺调制解调硬件电路的基础上,实现对不同长度环圈组件精密分频的目的,从而提高陀螺性能,可以有效提升三轴陀螺全温零偏重复性能。(The invention relates to a precision frequency division method of a triaxial fiber-optic gyroscope, which is characterized by comprising the following steps: the frequency division method comprises the following steps: 1) designing an external clock reference and a two-stage DCM; 2) performing two-stage DCM scheme time sequence processing; 3) precision frequency division improvement; 4) and calculating a frequency division parameter algorithm. The frequency divider is scientific and reasonable in design, and achieves the purpose of precisely dividing the frequency of the ring assemblies with different lengths on the basis of not changing a gyro modulation and demodulation hardware circuit, so that the performance of the gyro is improved, and the full-temperature zero-offset repetition performance of the triaxial gyro can be effectively improved.)

1. A three-axis fiber optic gyroscope precision frequency division method is characterized in that: the frequency division method comprises the following steps:

1) external clock reference and two-stage DCM design

The two-stage DCM resources are used for realizing more precise frequency division, the cascade connection of DCM signals can be used for carrying out two-stage amplification on an external input clock signal, the frequency multiplication coefficient is expanded to 0-1024 from the original 0-32, the frequency division coefficient is expanded to 0-1024 from the original 0-32, and the larger latitude is brought to ring assemblies adaptive to different eigenfrequencies;

2) two-stage DCM scheme timing processing

The LOCKED signal of the first-stage DCM is used as an enabling signal of the second-stage DCM, namely the LOCKED signal is set to be at a high level after the first-stage DCM clock finishes latching, and the LOCKED signal is used as a reset signal of the second-stage DCM to drive the second-stage DCM to start working, so that the working sequence of the timing sequence two-stage DCM is ensured;

3) precision frequency division improvement

On the basis of the step 2), 3 clock signals (1-1, 1-2, 1-3) output by the first-stage DCM are 3 same clocks, and the same three clocks are subjected to frequency multiplication again through the second-stage DCM respectively, so that the difficulty of selecting a frequency division and multiplication coefficient algorithm is simplified;

4) frequency division parameter algorithm calculation

Based on the DCM scheme in the step 2), after determining the eigenfrequency of the three ring assemblies and the external input crystal oscillator, performing enumeration calculation to obtain frequency division parameters meeting the requirements, and performing a large amount of enumeration operations on first-stage DCM parameters M and N and second-stage DCM parameters P1, P2, P3, Q1, Q2 and Q3 to respectively obtain three different modulation frequencies T1, T2 and T3; and the parameter is effective only when errors of T1, T2 and T3 and eigenfrequencies F1, F2 and F3 meet design requirements at the same time.

Technical Field

The invention belongs to the technical field of fiber optic gyroscopes, relates to three-axis fiber optic gyroscope precision frequency division, and particularly relates to a three-axis fiber optic gyroscope precision frequency division method.

Background

In the process of developing and producing the three-axis gyroscope, the inevitable problem is that the eigenfrequencies of three ring assemblies of the same gyroscope are different, and the difference mainly comes from two aspects:

1) firstly, in the process of winding the ring, because the winding precision is not enough, errors exist in the turns of different layers of optical fibers, or the winding errors caused by different diameters of the optical fibers, and the errors are reflected as the geometric length difference of the ring assembly;

2) and secondly, the difference caused by the difference of equivalent refractive indexes, even if the geometric lengths of the 3 loop component optical fibers are the same, the difference of the equivalent refractive indexes can cause the difference of eigenfrequency.

Above two kinds of errors can all make triaxial fiber optic gyroscope in the debugging process, if use same modulation frequency to demodulate three ring subassemblies, then the difference of modulation frequency and eigen frequency can lead to performance super poor such as top full temperature zero offset repeatability, influences the top precision.

At present, the frequency division schemes of the common three-axis gyroscope mainly include two types: firstly, 1 external input clock is used as a clock reference signal, frequency multiplication is carried out through a DCM (clock and data converter) module in the FPGA to obtain a modulation frequency, and three ring assemblies are demodulated; and secondly, an external clock signal is also used as a clock reference, and a DCM resource is used for outputting 3 modulation frequencies respectively corresponding to the eigenfrequencies of the 3 ring components. However, this solution has a great problem in applicability. In the use process of the internal DCM of the FPGA, if 3 clock signals need to be output, the three signals need to meet the principle of having the least common multiple. For three ring assemblies with different eigenfrequencies, it is difficult to require the least common multiple of three different modulation frequencies to satisfy the requirement of the DCM module (and the maximum multiplication factor is 32), so the scheme does not satisfy the engineering application condition.

Under the condition of not changing a hardware circuit, the scheme is improved, internal DCM module resources (taking Spartan-6 series chips as examples, 4 DCM resources are shared inside) of the FPGA are fully utilized, two-stage frequency multiplication processing is carried out on an external clock reference, and modulation and demodulation operation of any triaxial gyroscope can be realized by combining a corresponding algorithm.

Disclosure of Invention

The invention aims to overcome the defects of the prior art and provide a precise frequency division method of a triaxial fiber-optic gyroscope, which realizes the purpose of precisely dividing frequency of ring assemblies with different lengths on the basis of not changing a gyroscope modulation and demodulation hardware circuit, thereby improving the performance of the gyroscope.

The technical problem to be solved by the invention is realized by the following technical scheme:

a three-axis fiber optic gyroscope precision frequency division method is characterized in that: the frequency division method comprises the following steps:

1) external clock reference and two-stage DCM design

The two-stage DCM resources are used for realizing more precise frequency division, the cascade connection of DCM signals can be used for carrying out two-stage amplification on an external input clock signal, the frequency multiplication coefficient is expanded to 0-1024 from the original 0-32, the frequency division coefficient is expanded to 0-1024 from the original 0-32, and the larger latitude is brought to ring assemblies adaptive to different eigenfrequencies;

2) two-stage DCM scheme timing processing

The LOCKED signal of the first-stage DCM is used as an enabling signal of the second-stage DCM, namely the LOCKED signal is set to be at a high level after the first-stage DCM clock finishes latching, and the LOCKED signal is used as a reset signal of the second-stage DCM to drive the second-stage DCM to start working, so that the working sequence of the timing sequence two-stage DCM is ensured;

3) precision frequency division improvement

On the basis of the step 2), 3 clock signals (1-1, 1-2, 1-3) output by the first-stage DCM are 3 same clocks, and the same three clocks are subjected to frequency multiplication again through the second-stage DCM respectively, so that the difficulty of selecting a frequency division and multiplication coefficient algorithm is simplified;

4) frequency division parameter algorithm calculation

Based on the DCM scheme in the step 2), after determining the eigenfrequency of the three ring assemblies and the external input crystal oscillator, performing enumeration calculation to obtain frequency division parameters meeting the requirements, and performing a large amount of enumeration operations on first-stage DCM parameters M and N and second-stage DCM parameters P1, P2, P3, Q1, Q2 and Q3 to respectively obtain three different modulation frequencies T1, T2 and T3; and the parameter is effective only when errors of T1, T2 and T3 and eigenfrequencies F1, F2 and F3 meet design requirements at the same time.

The invention has the advantages and beneficial effects that:

1. the precise frequency division method of the triaxial fiber-optic gyroscope achieves the purpose of precisely dividing the frequency of the ring assemblies with different lengths on the basis of not changing a gyroscope modulation and demodulation hardware circuit, thereby improving the performance of the gyroscope.

Drawings

FIG. 1 is a diagram of a precision frequency division scheme of a triaxial fiber optic gyroscope of the prior art;

FIG. 2 is a diagram of a precision frequency division scheme of a triaxial fiber optic gyroscope according to the present invention;

FIG. 3 is a diagram of another triaxial fiber optic gyroscope precision frequency division scheme according to the present invention;

fig. 4 is a flow chart of the frequency division parameter algorithm of the present invention.

Detailed Description

The present invention is further illustrated by the following specific examples, which are intended to be illustrative, not limiting and are not intended to limit the scope of the invention.

A three-axis fiber optic gyroscope precision frequency division method is characterized in that: the frequency division method comprises the following steps:

1) external clock reference and two-stage DCM design

Since it is specified in the DCM resource usage rule inside the FPGA that when outputting 3 clocks using 1 DCM resource, the three clocks have the smallest common multiple, and the common multiple is less than 32, there is a great limitation in design.

Thus, a more sophisticated frequency division scheme can be achieved with two levels of DCM resources, as shown in fig. 2.

Through the cascade connection of DCM signals, the external input clock signals can be amplified in two stages, the frequency multiplication coefficient is expanded from original 0-32 to 0-1024, and the frequency division coefficient is also expanded from original 0-32 to 0-1024, so that greater latitude is brought to the ring component adaptive to different eigenfrequencies.

2) Two-stage DCM scheme timing processing

As shown in FIG. 2, since the DCM cascade scheme is used, the LOCKED signal of the first stage DCM is required to be used as the enable signal of the second stage DCM, so that the working sequence of the sequential two-stage DCM can be ensured. After the first-stage DCM clock finishes latching, the LOCKED signal is set to be at a high level and is used as a reset signal of the second-stage DCM to drive the second-stage DCM to start working.

3) Precision frequency division improvement

In the scheme of fig. 2, 3 clock signals (1-1, 1-2, 1-3) output by the first-stage DCM are 3 identical clocks, and the identical three clocks are frequency-multiplied by the second-stage DCM, so that the difficulty of selecting the frequency-division-multiplication-coefficient algorithm can be simplified to the greatest extent in the algorithm.

In extreme cases, if the error of the modulation frequency and the error of the eigen frequency are limited to 5Hz, the required division parameters cannot be calculated. There is therefore a need for an improvement to the solution of figure 2, as shown in figure 3.

In the scheme shown in fig. 3, the division coefficients N1, N2, and N3 of the 3 clock signals output by the first stage of DCM are different, so that the frequency output range is wider when the second stage of DCM frequency multiplication is performed, but the algorithm is more complicated.

4) Frequency division parameter algorithm calculation

Taking the frequency division scheme shown in fig. 2 as an example, after determining the eigenfrequencies of the three ring assemblies and the external input crystal oscillator, enumeration is performed to calculate the frequency division parameters meeting the requirements, and the flow chart of the algorithm is shown in fig. 4.

A large number of enumeration operations are carried out on the first-stage DCM parameters M and N and the second-stage DCM parameters P1, P2, P3, Q1, Q2 and Q3, and three different modulation frequencies T1, T2 and T3 are obtained respectively. This parameter is valid only if the errors of T1, T2, T3 and the eigenfrequencies F1, F2, F3 meet the design requirements at the same time.

Although the embodiments of the present invention and the accompanying drawings are disclosed for illustrative purposes, those skilled in the art will appreciate that: various substitutions, changes and modifications are possible without departing from the spirit and scope of the invention and the appended claims, and therefore the scope of the invention is not limited to the disclosure of the embodiments and the accompanying drawings.