阅读说明：本技术 一种旋转测向装置、系统及情报侦察设备 (Rotary direction finding device, system and information reconnaissance equipment ) 是由 方棉佳 王东风 熊子源 张云凯 杨海东 于 2020-04-22 设计创作，主要内容包括：本申请提供了一种旋转测向装置、系统及情报侦察设备,涉及电子信息技术领域,其中,旋转测向装置包括一维干涉仪和旋转伺服机构,一维干涉仪与旋转伺服机构的动力输出部连接,以使旋转伺服机构能够带动一维干涉仪旋转；由于一维干涉仪的测向精度高,所以一维干涉仪的应用较广泛,但是一维干涉仪阵的瞬时空域覆盖角度仅为90°左右,进而为了保证测向精度以及覆盖360°空域,在一维干涉仪的底部设置一个旋转伺服机构,旋转伺服机构的转动能够带动一维干涉仪进行转动,从而在保证满足旋转测向装置的测向精度以及覆盖360°空域的同时,减少设备量,使得情报侦察设备便于背负和机动,提高情报侦察设备的稳定性和可靠性。(The application provides a rotary direction-finding device, a rotary direction-finding system and information reconnaissance equipment, and relates to the technical field of electronic information, wherein the rotary direction-finding device comprises a one-dimensional interferometer and a rotary servo mechanism, and the one-dimensional interferometer is connected with a power output part of the rotary servo mechanism so that the rotary servo mechanism can drive the one-dimensional interferometer to rotate; because the direction-finding precision of one-dimensional interferometer is high, so the application of one-dimensional interferometer is more extensive, but the instantaneous airspace coverage angle of one-dimensional interferometer array is only about 90, and then in order to guarantee direction-finding precision and cover 360 airspaces, set up a rotatory servo mechanism in the bottom of one-dimensional interferometer, the rotation of rotatory servo mechanism can drive one-dimensional interferometer and rotate, thereby when guaranteeing to satisfy the direction-finding precision of rotatory direction-finding device and cover 360 airspaces, reduce the equipment volume, make information reconnaissance equipment be convenient for bear and maneuver, improve the stability and the reliability of information reconnaissance equipment.)

1. A rotary direction-finding device is characterized by comprising a one-dimensional interferometer and a rotary servo mechanism, wherein the one-dimensional interferometer is connected with a power output part of the rotary servo mechanism, so that the rotary servo mechanism can drive the one-dimensional interferometer to rotate.

2. The rotary direction-finding device of claim 1, wherein the rotary servo comprises a control member, a power member, and a transmission assembly, an output of the transmission assembly being configured as the power output;

the control piece is connected with the control end of the power piece, the output end of the power piece is connected with the input end of the transmission assembly, and the transmission assembly drives the one-dimensional interferometer to rotate under the driving of the power piece.

3. The rotary direction-finding device of claim 2, wherein the transmission assembly includes a worm gear and a worm that mesh with each other;

the power output part is formed on the surface of the worm wheel, and the one-dimensional interferometer is connected with the surface of the worm wheel; the worm is in transmission connection with the power part.

4. The rotary direction-finding device according to claim 3, wherein the rotary servo mechanism further comprises a limiting component, the limiting component comprises a limiting sheet and a limiting block, the limiting sheet is arranged on the side edge of the worm wheel, and the limiting block is arranged on one side of the worm wheel;

in the rotation process of the worm wheel, when the limiting piece is abutted to the limiting block, the limiting block can apply a force for preventing the limiting piece from continuing to rotate along the original direction.

5. The rotary direction-finding device according to claim 4, wherein the limiting assembly further comprises a limiting seat and a limiting rod, the limiting seat is arranged in the rotary servo mechanism and fixed relative to the housing of the rotary servo mechanism, and two ends of the limiting rod are arranged on the limiting seat; the limiting block is arranged on the limiting rod in a penetrating mode and can slide between the limiting seats along the limiting rod.

6. The rotary direction-finding device of claim 3, wherein the rotary servo mechanism further comprises position sensors distributed around the worm gear, and the position sensors are connected with the control member and used for acquiring position information of the rotation of the worm gear.

7. The rotary direction-finding device of claim 2, wherein the power member is a servo motor.

8. The rotary direction-finding device of claim 7, wherein the one-dimensional interferometer is connected to the rotary servo by one or more of a pin, a screw, and a stud.

9. A rotary direction finding system comprising a display control device and a rotary direction finding device according to any one of claims 1 to 8;

the display control device is in communication connection with a rotary servo mechanism of the rotary direction-finding device through a serial port or a network port and is used for controlling the action and starting and stopping of the servo mechanism.

10. An intelligence reconnaissance apparatus comprising a rotary direction finding device as claimed in any one of claims 1 to 8.

Technical Field

The application relates to the technical field of electronic information, in particular to a rotary direction-finding device, a rotary direction-finding system and information reconnaissance equipment.

Background

In the field of electronic information, a direction-finding precision index is an important technical index of electronic information equipment, and the traditional direction-finding methods comprise a rotating maximum value method, a range-comparison direction-finding method, a one-dimensional multi-baseline direction-finding method, a multi-dimensional multi-baseline interferometer direction-finding method and the like, and the direction-finding methods have advantages and disadvantages; however, in the case of a ground portable information reconnaissance apparatus, the portability of the apparatus must be considered in addition to the direction-finding accuracy index.

The existing ground portable information reconnaissance equipment adopts the traditional direction finding method, has poor direction finding precision and large equipment quantity, and is inconvenient to carry and maneuver.

Disclosure of Invention

In view of this, an object of the present application is to provide a rotary direction finding device, a rotary direction finding system and an information scouting apparatus, which can reduce the amount of apparatuses while ensuring the direction finding precision of the rotary direction finding device and covering 360 ° airspace, so that the information scouting apparatus is convenient to carry on the back and maneuver, and the stability and reliability of the information scouting apparatus are improved.

In a first aspect, an embodiment of the present application provides a rotary direction finding device, which includes a one-dimensional interferometer and a rotary servo mechanism, where the one-dimensional interferometer is connected to a power output portion of the rotary servo mechanism, so that the rotary servo mechanism can drive the one-dimensional interferometer to rotate.

Preferably, the rotary servo comprises a control member, a power member and a transmission assembly, the output end of the transmission assembly being constructed as the power output part;

the control piece is connected with the control end of the power piece, the output end of the power piece is connected with the input end of the transmission assembly, and the transmission assembly drives the one-dimensional interferometer to rotate under the driving of the power piece.

Preferably, the transmission assembly comprises a worm wheel and a worm which mesh with each other;

the power output part is formed on the surface of the worm wheel, and the one-dimensional interferometer is connected with the surface of the worm wheel; the worm is in transmission connection with the power part.

Preferably, the rotary servo mechanism further comprises a limiting assembly, the limiting assembly comprises a limiting sheet and a limiting block, the limiting sheet is arranged on the side edge of the worm wheel, and the limiting block is arranged on one side of the worm wheel;

in the rotation process of the worm wheel, when the limiting piece is abutted to the limiting block, the limiting block can apply a force for preventing the limiting piece from continuing to rotate along the original direction.

Preferably, the limiting assembly further comprises a limiting seat and a limiting rod, the limiting seat is arranged in the rotary servo mechanism and fixed relative to the shell of the rotary servo mechanism, and two ends of the limiting rod are arranged on the limiting seat; the limiting block is arranged on the limiting rod in a penetrating mode and can slide between the limiting seats along the limiting rod.

Preferably, the rotary servo mechanism further comprises position sensors distributed around the worm wheel, and the position sensors are connected with the control piece and used for acquiring the position information of the rotation of the worm wheel.

Preferably, the power member is a servo motor.

Preferably, the one-dimensional interferometer is connected to the rotary servo by one or more of a pin, a screw and a stud.

In a second aspect, the present application provides a rotary direction finding system, including a display control device and the rotary direction finding device as described above;

the display control device is in communication connection with a rotary servo mechanism of the rotary direction-finding device through a serial port or a network port and is used for controlling the action and starting and stopping of the servo mechanism.

In a third aspect, an embodiment of the present application provides an intelligence reconnaissance apparatus, including a rotary direction finding device as described above.

The embodiment of the application provides a rotatory direction finding device, system and information reconnaissance equipment, wherein, rotatory direction finding device includes one-dimensional interferometer and rotatory servo, and the one-dimensional interferometer is connected with rotatory servo's power take off to make rotatory servo can drive the one-dimensional interferometer rotatory. The one-dimensional interferometer is wide in application due to high direction-finding precision, but the instantaneous airspace coverage angle of the one-dimensional interferometer array is only about 90 degrees, and further, in order to ensure the direction-finding precision and cover the airspace of 360 degrees, a rotary servo mechanism is arranged at the bottom of the one-dimensional interferometer, and the rotation of the rotary servo mechanism can drive the one-dimensional interferometer to rotate, so that the detection and the direction-finding of an empty target are realized; the technical scheme of this application when guaranteeing to satisfy the direction finding precision of rotatory direction-finding device and cover 360 airspaces, has reduced the equipment volume for information reconnaissance equipment is convenient for bear and maneuver, improves the stability and the reliability of information reconnaissance equipment.

In order to make the aforementioned objects, features and advantages of the present application more comprehensible, preferred embodiments accompanied with figures are described in detail below.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present application and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained from the drawings without inventive effort.

Fig. 1 is a schematic structural diagram of a rotary direction-finding device according to an embodiment of the present disclosure;

FIG. 2 is a schematic diagram of a one-dimensional interferometer provided by an embodiment of the present application;

fig. 3 is an internal schematic view of a rotary servo mechanism according to an embodiment of the present disclosure.

Reference numerals:

10-one-dimensional interferometer; 20-a rotary servo mechanism; 201-a transmission assembly; 202-a limiting block; 203-limiting piece; 204-position sensor.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only a part of the embodiments of the present application, and not all the embodiments. The components of the embodiments of the present application, generally described and illustrated in the figures herein, can be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of the present application, presented in the accompanying drawings, is not intended to limit the scope of the claimed application, but is merely representative of selected embodiments of the application. All other embodiments, which can be derived by a person skilled in the art from the embodiments of the present application without making any creative effort, shall fall within the protection scope of the present application.

In the description of the embodiments of the present application, it should be noted that the terms "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings or orientations or positional relationships that the products of the present invention are usually placed in when used, and are only used for convenience of describing the present invention and simplifying the description, but do not indicate or imply that the devices or elements indicated must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.

Furthermore, the terms "horizontal", "vertical" and the like do not imply that the components are required to be absolutely horizontal or pendant, but rather may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.

In the description of the embodiments of the present application, it should also be noted that, unless otherwise explicitly stated or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.

In a first aspect, an embodiment of the present application provides a rotary direction-finding device, please refer to fig. 1, where fig. 1 is a schematic structural diagram of the rotary direction-finding device provided in the embodiment of the present application; as shown in fig. 1, the rotary direction-finding device provided in the embodiment of the present application includes a one-dimensional interferometer 10 and a rotary servo 20, where the one-dimensional interferometer 10 is connected to a power output portion of the rotary servo 20, so that the rotary servo 20 can rotate the one-dimensional interferometer 10.

Wherein, the one-dimensional interferometer 10 is connected with the rotary servo 20 through one or more of pins, screws and studs.

In the embodiment of the present application, the one-dimensional interferometer 10 is located above the rotary servo mechanism 20, and the peripheries of the one-dimensional interferometer 10 and the rotary servo mechanism 20 are respectively connected by four screws, so that the one-dimensional interferometer 10 and the rotary servo mechanism 20 are fixedly connected, and the stability of the rotary direction-finding device can be improved.

The one-dimensional interferometer 10 is connected with a power output part of the rotary servo mechanism 20, so that when the rotary servo mechanism 20 rotates, the one-dimensional interferometer 10 can be driven to rotate along with the rotary servo mechanism 20, the aerial target can be detected and received and the direction can be detected, and the real-time motion track of the aerial signal can be given.

Referring to fig. 2, fig. 2 is a schematic diagram of a one-dimensional interferometer according to an embodiment of the present disclosure; as shown in fig. 2, 4 base lines are arranged at a certain distance, the distance between every two antennas is a base line, the direction-finding accuracy is related to the longest base line, the direction-finding accuracy of the one-dimensional interferometer is generally about 1.5 ° (RMS), and the accuracy may be different when the frequency is different.

When the distance between the radiation source and the antenna array is much larger than the spacing between the antennas, the signals from the same radiation source incident on the respective antennas are approximately parallel waves. Assuming that the angle between the incident signal and the visual axis of the antenna is θ, the phase difference between the signals received by two adjacent antennas can be expressed as:

wherein:is the phase difference between the two antennas, andN_iis an integer and λ is the wavelength of the incident signal.

If the signal wavelength λ is known, the phase difference can be determined by using equation (1)Calculating the azimuth angle theta of the signal:

since phase measuring devices are usually modulo 2 pi, only phase values in the range of 2 pi can be measuredAnd the integer N cannot be determined_i. Thus, due to N_iIs not determined, by equation (2), for oneThere will be multiple azimuth angles corresponding to it, making the direction finding result ambiguous.

One method for resolving ambiguity of a one-dimensional multi-baseline interferometer is to use a short baseline to make the shortest baseline length less than half of the signal wavelength, and the required shortest baseline length is shorter as the signal frequency is increased. In the ambiguity resolution process, through the matching of the virtual baseline and the actual baseline, the phase ambiguity is resolved by using the shorter virtual baseline, the direction-finding precision is ensured through the long baseline, and the final azimuth angle theta is determined.

However, the instantaneous airspace coverage angle of the one-dimensional multi-baseline interferometer is about 90 degrees, and after the equipment is fixed, the equipment cannot cover a 360-degree airspace.

In order to guarantee to satisfy one-dimensional interferometer's direction finding precision and cover 360 airspaces, reduce the equipment volume for information reconnaissance equipment is convenient for bear and maneuver, improves information reconnaissance equipment's stability and reliability, this application provides foretell rotatory direction finding device, including one-dimensional interferometer and rotatory servo mechanism, the one-dimensional interferometer is connected with rotatory servo mechanism's power take off portion, and rotatory servo mechanism can drive the one-dimensional interferometer rotatory, and then solves the technical problem that the aforesaid exists. In addition, the equipment amount is reduced, the equipment can be transported by roads and railways, and the equipment can be carried on the back by people in places where vehicles cannot reach.

The rotary servo mechanism comprises a control part, a power part and a transmission component, wherein the output end of the transmission component is constructed as a power output part;

the control part is connected with the control end of the power part, the output end of the power part is connected with the input end of the transmission assembly, and the transmission assembly drives the one-dimensional interferometer to rotate under the driving of the power part.

In the embodiment of the application, the control part is a circuit board, the power part is a servo motor, and the circuit board is electrically connected with a control end of the servo motor so that the circuit board can control the operation of the servo motor; the output end of the servo motor is connected with the input end of the transmission assembly, the transmission assembly drives the one-dimensional interferometer to rotate under the driving of the servo motor, and the servo motor is adopted in the application because the accuracy of the control speed and the position of the servo motor is high.

Referring to fig. 3, fig. 3 is an internal schematic view of a rotary servo mechanism according to an embodiment of the present disclosure. As shown in fig. 3, the transmission assembly 201 includes a worm wheel and a worm that mesh with each other;

the surface of the worm wheel forms a power output part, and the one-dimensional interferometer is connected with the surface of the worm wheel; the worm is in transmission connection with the power part.

In this application embodiment, servo motor's output is connected with the worm transmission, and then servo motor drives the worm and is rotary motion, worm and turbine intermeshing to rotary motion is also done to the turbine under the drive of worm, and the surface and the one-dimensional interferometer of worm wheel are connected, thereby realize that the one-dimensional interferometer is rotary motion under the drive of turbine.

The one-dimensional interferometer is connected with the rotary servo mechanism through one or more of pins, screws and studs.

Specifically, four through holes are uniformly formed in the circumferential direction of a turbine of the rotary servo mechanism, the four through holes are also formed in the positions, corresponding to the turbine of the rotary servo mechanism, of the one-dimensional interferometer, screws are arranged in the through holes, and the one-dimensional interferometer is connected with the rotary servo mechanism through the screws, so that the stability of equipment is improved.

The rotary servo mechanism further comprises a limiting assembly, the limiting assembly comprises a limiting sheet 203 and a limiting block 202, the limiting sheet 203 is arranged on the side edge of the worm wheel, and the limiting block 202 is arranged on one side of the worm wheel; in the rotation process of the worm wheel, when the limiting piece 203 abuts against the limiting block 202, the limiting block 202 can apply a force to the limiting piece 203 to prevent the limiting piece from continuing to rotate in the original direction.

Furthermore, in the rotation process of the turbine, when the limiting piece 203 on the turbine contacts with the limiting block 202 on the shell of the rotary servo mechanism, the limiting block 202 can prevent the turbine from continuing to rotate along the same direction, and after the limiting piece 203 contacts with the limiting block 202, the turbine starts to rotate in the opposite direction until the limiting piece 203 on the turbine returns to the initial position, then starts to rotate, and continues the process, so that the effect that the rotary servo mechanism drives the one-dimensional interferometer to rotate is achieved.

The limiting assembly of the embodiment of the application further comprises a limiting seat and a limiting rod, the limiting seat is arranged in the rotary servo mechanism and fixed relative to the shell of the rotary servo mechanism, and two ends of the limiting rod are arranged on the limiting seat; the limiting block is arranged on the limiting rod in a penetrating mode and can slide between the limiting seats along the limiting rod.

The rotary servo mechanism further comprises position sensors 204 distributed around the worm wheel, and the position sensors 204 are connected with the control piece and used for acquiring the position information of the rotation of the worm wheel.

According to the embodiment of the application, the position sensors 204 are arranged on the periphery of the worm wheel, the position information of the rotation of the turbine is detected in real time through the position sensors 204, and the detection result is sent to the control part, so that the control part controls the rotation condition of the turbine in real time according to the detection result.

As can be seen from fig. 3, the rotary servo mechanism provided in the embodiment of the present application realizes 270 ° rotation of the rotary servo mechanism through position detection of the position sensor 204 and cooperation between the limiting plate 203 and the limiting block 202, so as to compensate rotation of the one-dimensional interferometer, so that the one-dimensional interferometer realizes 360 ° rotation, and further covers 360 ° airspace.

According to the embodiment of the application, the one-dimensional interferometer and the rotary servo mechanism are combined for use, so that the one-dimensional interferometer is high in direction finding precision and good in real-time performance when the direction finding is carried out, and accurate direction information of a target can be provided; by rotating the servo mechanism, the problem of forward and backward blurring of the one-dimensional interferometer array can be solved, and a real-time motion track of an aerial target can be given; meanwhile, the equipment quantity is small, and the ground equipment is convenient to maneuver and erect.

Based on the same technical concept, the embodiment of the application also provides a rotary direction finding system, which comprises a display control device and the rotary direction finding device;

the display control device is in communication connection with a rotary servo mechanism of the rotary direction-finding device through a serial port or a network port and is used for controlling parameter modification and starting and stopping of the servo mechanism.

When the equipment is in operation, the rotation angle and the rotation speed of the rotation servo mechanism can be controlled on the display control device according to needs, display control software in the display control device issues commands to the signal processing module, and the signal processing module is communicated with the rotation servo mechanism through a serial port to realize the control of the rotation servo mechanism.

Since the rotary direction-finding device has the technical effects, the rotary direction-finding system with the rotary direction-finding device also has the same technical effects, and the same structure and technical effects are not repeated herein.

In conclusion, the rotary direction finding is realized by combining a one-dimensional multi-baseline interferometer array with a rotary servo mechanism, and the device is divided into two one-dimensional multi-baseline interferometer arrays for covering a frequency range of 0.8-18 GHz (which can be expanded according to actual needs), wherein one interferometer array covers 0.8-6 GHz, and the other interferometer array covers 6-18 GHz; each array is provided with 4-5 unit antennas, and the effect of covering 360-degree airspace range is achieved by utilizing the instantaneous 90-degree airspace visual angle of a one-dimensional interferometer array and combining a rotary servo mechanism; the rotary servo mechanism adopts a program control mode, the equipment comprises a display control device, the display control device is communicated with the rotary servo mechanism through a serial port or a network port, a control interface for controlling the rotary servo mechanism is arranged in control software of the display control device, and an operator operates the rotary servo mechanism through setting and operating commands of the rotary servo mechanism in the control interface, such as rotation rate, rotation direction, rotation stepping, stopping and the like, so as to achieve the purpose of controlling the rotation of the interferometer array.

Based on the same technical concept, the embodiment of the present application further provides an information reconnaissance apparatus, including the above-described rotary direction-finding device.

The embodiment of the application organically combines the one-dimensional interferometer and the rotary servo mechanism, thereby solving the difficulty in the design of the conventional ground electronic information reconnaissance equipment, the invention is verified and used by engineering, the direction-finding precision is about 1.0 degree (RMS) in the whole frequency band, and the weight is 14 kilograms; this application had both guaranteed the direction finding precision of portable information reconnaissance equipment in ground, the position information of the target of giving that again can be accurate, and the stability and the reliability of equipment have been improved to the flexible and of being convenient for bear simultaneously.

Since the rotary direction-finding device has the technical effects, the information reconnaissance equipment with the rotary direction-finding device also has the same technical effects, and the same structure and technical effects are not repeated herein.

The rotary direction-finding device comprises a one-dimensional interferometer and a rotary servo mechanism, wherein the one-dimensional interferometer is connected with a power output part of the rotary servo mechanism, so that the rotary servo mechanism can drive the one-dimensional interferometer to rotate. The one-dimensional interferometer is wide in application due to high direction-finding precision, but the instantaneous airspace coverage angle of the one-dimensional interferometer array is only about 90 degrees, and further, in order to ensure the direction-finding precision and cover the airspace of 360 degrees, a rotary servo mechanism is arranged at the bottom of the one-dimensional interferometer, and the rotation of the rotary servo mechanism can drive the one-dimensional interferometer to rotate, so that the detection and the direction-finding of an empty target are realized; the technical scheme of this application when guaranteeing to satisfy the direction finding precision of rotatory direction-finding device and cover 360 airspaces, has reduced the equipment volume for information reconnaissance equipment is convenient for bear and maneuver, improves the stability and the reliability of information reconnaissance equipment.

Finally, it should be noted that: the above-mentioned embodiments are only specific embodiments of the present application, and are used for illustrating the technical solutions of the present application, but not limiting the same, and the scope of the present application is not limited thereto, and although the present application is described in detail with reference to the foregoing embodiments, those skilled in the art should understand that: any person skilled in the art can modify or easily conceive the technical solutions described in the foregoing embodiments or equivalent substitutes for some technical features within the technical scope disclosed in the present application; such modifications, changes or substitutions do not depart from the spirit and scope of the exemplary embodiments of the present application, and are intended to 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.