CN110717234A - Irregular layout triple angular position simulation method, system and medium - Google Patents

Irregular layout triple angular position simulation method, system and medium Download PDF

Info

Publication number
CN110717234A
CN110717234A CN201910989778.2A CN201910989778A CN110717234A CN 110717234 A CN110717234 A CN 110717234A CN 201910989778 A CN201910989778 A CN 201910989778A CN 110717234 A CN110717234 A CN 110717234A
Authority
CN
China
Prior art keywords
antenna
triple
target
calibration device
calibration
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201910989778.2A
Other languages
Chinese (zh)
Inventor
陆戈辉
王立权
唐成师
柴娟芳
闫宏雁
黄杉
孟宇麟
郝恩义
徐啸
赵吕懿
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Institute of Electromechanical Engineering
Original Assignee
Shanghai Institute of Electromechanical Engineering
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanghai Institute of Electromechanical Engineering filed Critical Shanghai Institute of Electromechanical Engineering
Priority to CN201910989778.2A priority Critical patent/CN110717234A/en
Publication of CN110717234A publication Critical patent/CN110717234A/en
Pending legal-status Critical Current

Links

Images

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

The invention provides a method, a system and a medium for simulating an irregular layout triple angular position, which comprise the following steps: designing a calibration device: manufacturing a calibration device according to the working frequency band of the antenna array, and receiving the radiation signal of the antenna by using the manufactured calibration device; a calibration table generation step: according to the manufactured calibration device, the antenna position deviation of the antenna array is obtained through testing, an antenna position calibration table is generated, and the antenna position calibration table is led into target control software; a triple judgment step: judging the triple where the target is located again according to the actual equivalent position of the antenna by a triangular area positioning method; amplitude distribution step: and redistributing the amplitude of the triple antenna through an amplitude gravity center formula according to the position of the triple antenna where the target is located, which is obtained through redetermination. The invention can improve the radio frequency target simulation precision of the semi-physical simulation system, and has the advantages of simple realization, low manufacturing cost and easy later modification.

Description

Irregular layout triple angular position simulation method, system and medium
Technical Field
The invention relates to the technical field of simulation, in particular to a method, a system and a medium for simulating an irregular layout triple corner position.
Background
In order to meet the increasing simulation requirements, simulation conditions such as microwave/millimeter wave compounding, radio frequency/infrared compounding and the like need to be realized in a darkroom, so that corresponding equipment such as a small array, a beam synthesizer and the like in the darkroom can cause the change of the darkroom environment, and the influences of multipath effect, diffraction and the like are generated. Therefore, the equivalent angular position of each antenna measured by the calibration device greatly deviates from the theoretical value, and the deviation is different at different frequency points.
Patent document CN 208477019U discloses a microwave darkroom. The antenna position error has great influence on the target simulation precision, and a method of adjusting a six-degree-of-freedom adjuster is adopted to ensure that the physical position deviation of the antenna is within an allowable range through optical calibration. However, under the condition that the physical position of the antenna is not changed, the equivalent angular position deviation of the antenna caused by the change of the darkroom environment changes along with the change of the frequency, so the traditional optical calibration method has poor effect of correcting the position error of the antenna.
Disclosure of Invention
In view of the defects in the prior art, an object of the present invention is to provide a method, a system and a medium for simulating an irregular layout triple angular position.
The invention provides an irregular layout triple angular position simulation method, which comprises the following steps:
designing a calibration device: manufacturing a calibration device according to the working frequency band of the antenna array, and receiving the radiation signal of the antenna by using the manufactured calibration device;
a calibration table generation step: according to the manufactured calibration device, the antenna position deviation of the antenna array is obtained through testing, an antenna position calibration table is generated, and the antenna position calibration table is led into target control software;
a triple judgment step: judging the triple where the target is located again according to the actual equivalent position of the antenna by a triangular area positioning method;
amplitude distribution step: and redistributing the amplitude of the triple antenna through an amplitude gravity center formula according to the position of the triple antenna where the target is located, which is obtained through redetermination.
Preferably, the calibration device comprises: the system comprises a receiving antenna, a microwave cable and a vector network analyzer;
the receiving antenna is connected with the vector network analyzer through the microwave cable.
Preferably, the receiving antennas include 4, 2 of which are disposed in the horizontal direction, and the other 2 are disposed in the elevation direction;
the vector network analyzer measures the phase difference of 2 receiving antennas arranged in the horizontal direction and the phase difference of 2 receiving antennas arranged in the pitching direction, so that the antenna position deviation in the horizontal direction and the pitching direction is obtained.
Preferably, the triple determining step includes:
and judging whether the target D is in a triangle ABC formed by the first triple: and calculating the directed areas of the triangles ABD, DBC and ADC, if the directed areas of the triangles ABD, DBC and ADC are all larger than 0 or all smaller than 0, indicating that the target D is in the first triple, otherwise, judging whether the target D is in the next triple in the same way.
According to the invention, the irregular layout triple angular position simulation system comprises:
a calibration device design module: manufacturing a calibration device according to the working frequency band of the antenna array, and receiving the radiation signal of the antenna by using the manufactured calibration device;
a calibration table generation module: according to the manufactured calibration device, the antenna position deviation of the antenna array is obtained through testing, an antenna position calibration table is generated, and the antenna position calibration table is led into target control software;
a triple determination module: judging the triple where the target is located again according to the actual equivalent position of the antenna by a triangular area positioning method;
an amplitude allocation module: and redistributing the amplitude of the triple antenna through an amplitude gravity center formula according to the position of the triple antenna where the target is located, which is obtained through redetermination.
Preferably, the calibration device comprises: the system comprises a receiving antenna, a microwave cable and a vector network analyzer;
the receiving antenna is connected with the vector network analyzer through the microwave cable.
Preferably, the receiving antennas include 4, 2 of which are disposed in the horizontal direction, and the other 2 are disposed in the elevation direction;
the vector network analyzer measures the phase difference of 2 receiving antennas arranged in the horizontal direction and the phase difference of 2 receiving antennas arranged in the pitching direction, so that the antenna position deviation in the horizontal direction and the pitching direction is obtained.
Preferably, the triple determination module includes:
and judging whether the target D is in a triangle ABC formed by the first triple: and calculating the directed areas of the triangles ABD, DBC and ADC, if the directed areas of the triangles ABD, DBC and ADC are all larger than 0 or all smaller than 0, indicating that the target D is in the first triple, otherwise, judging whether the target D is in the next triple in the same way.
According to the present invention, there is provided a computer readable storage medium storing a computer program which, when executed by a processor, implements the steps of the irregular layout triplet angular position simulation method described above.
Compared with the prior art, the invention has the following beneficial effects:
the invention can improve the radio frequency target simulation precision of the semi-physical simulation system, and has the advantages of simple realization, low manufacturing cost and easy later modification.
Drawings
Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:
FIG. 1 is a flow chart of the present invention;
fig. 2 is a schematic diagram of the positioning method of the present invention.
Detailed Description
The present invention will be described in detail with reference to specific examples. The following examples will assist those skilled in the art in further understanding the invention, but are not intended to limit the invention in any way. It should be noted that it would be obvious to those skilled in the art that various changes and modifications can be made without departing from the spirit of the invention. All falling within the scope of the present invention.
As shown in fig. 1, the method for simulating an irregular layout triplet angular position provided by the present invention includes:
designing a calibration device: and manufacturing a calibration device according to the working frequency band of the antenna array, and receiving the radiation signal of the antenna by using the manufactured calibration device.
A calibration table generation step: and testing according to the manufactured calibration device to obtain the antenna position deviation of the antenna array, generating an antenna position calibration table, and importing the antenna position calibration table into target control software.
A triple judgment step: and re-judging the triple of the target according to the actual equivalent position of the antenna by a triangular area positioning method.
Amplitude distribution step: and redistributing the amplitude of the triple antenna through an amplitude gravity center formula according to the position of the triple antenna where the target is located, which is obtained through redetermination.
As shown in fig. 2, the solid dots are the actual positions of each antenna in the antenna array, the hollow circles are the positions of the target D, and the numbers 1 to 13 are 13 triples in which the target D may be located.
The working process is as follows:
1) the calibration device is designed and manufactured according to the working frequency band of the antenna array, and mainly comprises a receiving antenna, a microwave cable and a vector network analyzer, wherein the receiving antenna is connected with the vector network analyzer through the microwave cable. The number of the receiving antennas is 4, the number of the receiving antennas is 2 in the horizontal direction, the number of the receiving antennas is 2 in the pitching direction, and the vector network analyzer sequentially measures the phase difference of the 2 receiving antennas in the horizontal direction and the phase difference of the 2 receiving antennas in the pitching direction to obtain the position deviation of the horizontal direction and the pitching direction of the antennas.
2) The antenna position deviation is obtained through the test of the designed calibration device, then an antenna position calibration table is generated, and the table is imported into a target control computer to be used by target control software.
3) Due to the fact that the actual position of the antenna changes, the target can run into an adjacent triple from the original triple, and the triple where the target is located is judged again according to the actual equivalent position of the antenna through a triangle area positioning method. As shown in fig. 2, an object D may appear in the triples 1,2, … …,13, and to determine whether the object is in the triplet 1 by the triangle area location method, only the directional areas of the triangles ABD, DBC and ADC need to be calculated, and if the three triangle areas are all larger than 0 (if the triangle ABC is an inverted triangle, here, smaller than 0), D is indicated as being within the triangle ABC, that is, the object is within the triplet. If the target is not in the triple, judging whether the target is in the next triple by the same method;
4) and redistributing the amplitude of the triple antenna through an amplitude gravity center formula according to the position of the triple antenna where the target is located. If the position of triad antenna A, B, C is expressed in terms of azimuth and elevation angles
Figure BDA0002237881630000041
θA
Figure BDA0002237881630000042
θB
Figure BDA0002237881630000043
θCThe target position isθDLet the amplitude assigned by triad antenna A, B, C be PA、PB、PCThen, according to the amplitude gravity center formula, the following can be obtained:
PA+PB+PC=1
PA·θA+PB·θB+PC·θC=θD
the amplitude of the triple antenna A, B, C may be obtained by solving a system of quadratic ternary equations.
And (3) experimental comparison: in a certain semi-physical simulation system, at a certain frequency point, because a beam synthesizer is added in a darkroom, the angle measurement error is changed from 0.12 degrees to 0.42 degrees through the measurement of a calibration device, and the simulation precision of a radio frequency target is greatly reduced; after the angular position simulation method is adopted, the angle measurement error is reduced from 0.42 degrees to 0.10 degrees, the simulation precision of the radio frequency target is greatly improved, and the method is slightly better than that before a beam synthesizer is installed, and the expected target is achieved.
On the basis of the irregular layout triple angular position simulation method, the invention also provides an irregular layout triple angular position simulation system, which comprises:
a calibration device design module: manufacturing a calibration device according to the working frequency band of the antenna array, and receiving the radiation signal of the antenna by using the manufactured calibration device;
a calibration table generation module: according to the manufactured calibration device, the antenna position deviation of the antenna array is obtained through testing, an antenna position calibration table is generated, and the antenna position calibration table is led into target control software;
a triple determination module: judging the triple where the target is located again according to the actual equivalent position of the antenna by a triangular area positioning method;
an amplitude allocation module: and redistributing the amplitude of the triple antenna through an amplitude gravity center formula according to the position of the triple antenna where the target is located, which is obtained through redetermination.
The present invention also provides a computer readable storage medium storing a computer program which, when executed by a processor, implements the steps of the irregular layout triplet angular position simulation method described above.
Those skilled in the art will appreciate that, in addition to implementing the system and its various devices, modules, units provided by the present invention as pure computer readable program code, the system and its various devices, modules, units provided by the present invention can be fully implemented by logically programming method steps in the form of logic gates, switches, application specific integrated circuits, programmable logic controllers, embedded microcontrollers and the like. Therefore, the system and various devices, modules and units thereof provided by the invention can be regarded as a hardware component, and the devices, modules and units included in the system for realizing various functions can also be regarded as structures in the hardware component; means, modules, units for performing the various functions may also be regarded as structures within both software modules and hardware components for performing the method.
The foregoing description of specific embodiments of the present invention has been presented. It is to be understood that the present invention is not limited to the specific embodiments described above, and that various changes or modifications may be made by one skilled in the art within the scope of the appended claims without departing from the spirit of the invention. The embodiments and features of the embodiments of the present application may be combined with each other arbitrarily without conflict.

Claims (9)

1. A method for modeling an irregular layout triplet angular position, comprising:
designing a calibration device: manufacturing a calibration device according to the working frequency band of the antenna array, and receiving the radiation signal of the antenna by using the manufactured calibration device;
a calibration table generation step: according to the manufactured calibration device, the antenna position deviation of the antenna array is obtained through testing, an antenna position calibration table is generated, and the antenna position calibration table is led into target control software;
a triple judgment step: judging the triple where the target is located again according to the actual equivalent position of the antenna by a triangular area positioning method;
amplitude distribution step: and redistributing the amplitude of the triple antenna through an amplitude gravity center formula according to the position of the triple antenna where the target is located, which is obtained through redetermination.
2. The method of irregular layout triplet angular position simulation of claim 1 wherein the calibration means comprises: the system comprises a receiving antenna, a microwave cable and a vector network analyzer;
the receiving antenna is connected with the vector network analyzer through the microwave cable.
3. The method of claim 2, wherein the receiving antennas comprise 4, 2 of which are disposed in a horizontal direction and the other 2 of which are disposed in a vertical direction;
the vector network analyzer measures the phase difference of 2 receiving antennas arranged in the horizontal direction and the phase difference of 2 receiving antennas arranged in the pitching direction, so that the antenna position deviation in the horizontal direction and the pitching direction is obtained.
4. The method of irregular layout triplet angular position simulation of claim 3, wherein the triplet decision step comprises:
and judging whether the target D is in a triangle ABC formed by the first triple: and calculating the directed areas of the triangles ABD, DBC and ADC, if the directed areas of the triangles ABD, DBC and ADC are all larger than 0 or all smaller than 0, indicating that the target D is in the first triple, otherwise, judging whether the target D is in the next triple in the same way.
5. An irregular layout triplet angular position simulation system comprising:
a calibration device design module: manufacturing a calibration device according to the working frequency band of the antenna array, and receiving the radiation signal of the antenna by using the manufactured calibration device;
a calibration table generation module: according to the manufactured calibration device, the antenna position deviation of the antenna array is obtained through testing, an antenna position calibration table is generated, and the antenna position calibration table is led into target control software;
a triple determination module: judging the triple where the target is located again according to the actual equivalent position of the antenna by a triangular area positioning method;
an amplitude allocation module: and redistributing the amplitude of the triple antenna through an amplitude gravity center formula according to the position of the triple antenna where the target is located, which is obtained through redetermination.
6. The system according to claim 5, wherein the calibration means comprises: the system comprises a receiving antenna, a microwave cable and a vector network analyzer;
the receiving antenna is connected with the vector network analyzer through the microwave cable.
7. The system according to claim 6, wherein the receiving antennas comprise 4, 2 of which are disposed in a horizontal direction and the other 2 are disposed in a vertical direction;
the vector network analyzer measures the phase difference of 2 receiving antennas arranged in the horizontal direction and the phase difference of 2 receiving antennas arranged in the pitching direction, so that the antenna position deviation in the horizontal direction and the pitching direction is obtained.
8. The irregular layout triplet angular position simulation system of claim 7 wherein the triplet decision module comprises:
and judging whether the target D is in a triangle ABC formed by the first triple: and calculating the directed areas of the triangles ABD, DBC and ADC, if the directed areas of the triangles ABD, DBC and ADC are all larger than 0 or all smaller than 0, indicating that the target D is in the first triple, otherwise, judging whether the target D is in the next triple in the same way.
9. A computer-readable storage medium storing a computer program, wherein the computer program, when executed by a processor, implements the steps of the irregular layout triplet angular position simulation method of any of claims 1 to 4.
CN201910989778.2A 2019-10-17 2019-10-17 Irregular layout triple angular position simulation method, system and medium Pending CN110717234A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910989778.2A CN110717234A (en) 2019-10-17 2019-10-17 Irregular layout triple angular position simulation method, system and medium

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910989778.2A CN110717234A (en) 2019-10-17 2019-10-17 Irregular layout triple angular position simulation method, system and medium

Publications (1)

Publication Number Publication Date
CN110717234A true CN110717234A (en) 2020-01-21

Family

ID=69212772

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910989778.2A Pending CN110717234A (en) 2019-10-17 2019-10-17 Irregular layout triple angular position simulation method, system and medium

Country Status (1)

Country Link
CN (1) CN110717234A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111562445A (en) * 2020-05-06 2020-08-21 中国人民解放军63892部队 Real-time monitoring method for angular simulation precision of radio frequency simulation test system

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001011719A1 (en) * 1999-08-10 2001-02-15 China Academy Of Telecommunications Technology,Mii Method and apparatus for calibrating smart antenna array
CN102590795A (en) * 2012-02-29 2012-07-18 中国电子科技集团公司第二十二研究所 Microwave scattering property test system based on vector network analyzer
CN103634903A (en) * 2013-11-22 2014-03-12 中国人民解放军理工大学 Noise canceling and positioning method of low-power-consumption small-scale equipment
CN104391187A (en) * 2014-09-18 2015-03-04 中国人民解放军63892部队 Alignment calibration device and alignment calibration method of multi-frequency-point antenna array
CN106209269A (en) * 2016-07-27 2016-12-07 华东师范大学 The calibration steps of sphere composite array near-field effect in a kind of radio freqency simulation system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001011719A1 (en) * 1999-08-10 2001-02-15 China Academy Of Telecommunications Technology,Mii Method and apparatus for calibrating smart antenna array
CN102590795A (en) * 2012-02-29 2012-07-18 中国电子科技集团公司第二十二研究所 Microwave scattering property test system based on vector network analyzer
CN103634903A (en) * 2013-11-22 2014-03-12 中国人民解放军理工大学 Noise canceling and positioning method of low-power-consumption small-scale equipment
CN104391187A (en) * 2014-09-18 2015-03-04 中国人民解放军63892部队 Alignment calibration device and alignment calibration method of multi-frequency-point antenna array
CN106209269A (en) * 2016-07-27 2016-12-07 华东师范大学 The calibration steps of sphere composite array near-field effect in a kind of radio freqency simulation system

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
刘力珲: "目标阵列校准技术的研究" *
唐蔚: "不规则波与开孔沉箱作用的数值研究" *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111562445A (en) * 2020-05-06 2020-08-21 中国人民解放军63892部队 Real-time monitoring method for angular simulation precision of radio frequency simulation test system
CN111562445B (en) * 2020-05-06 2022-08-19 中国人民解放军63892部队 Real-time monitoring method for angular simulation precision of radio frequency simulation test system

Similar Documents

Publication Publication Date Title
CN106209269B (en) The calibration method of spherical surface composite array near-field effect in a kind of radio freqency simulation system
US11309977B2 (en) Calibration method and communications device
US10302735B2 (en) Wireless terminal antenna directional characteristic measurement system and wireless terminal antenna directional characteristic measurement method
WO2020001661A1 (en) Measuring method and device
CN110646772B (en) Radar installation parameter calibration method and device
CN110568413A (en) test system and method integrating radar calibration, active transceiving and measurement parameters
CN105718662B (en) Characteristics of conformal array antenna structure tolerance fast determination method based on mechanical-electric coupling
CN104933213A (en) Large-scale phased antenna array wide-angle scanning optimization method based on space mapping
CN105527598B (en) A kind of field sensor calibration system and method
CN110717234A (en) Irregular layout triple angular position simulation method, system and medium
WO2020125349A1 (en) Field strength testing method
KR101744131B1 (en) Method for Designing and Evaluating Electromagnetic Anechoic Chamber in Virtual Space
CN113419208B (en) Interference source real-time direction finding method and device, storage medium and electronic equipment
CN108761279B (en) Polar coordinate grid searching method and system for positioning partial discharge source
CN103840872A (en) Device and method for generating weight of antenna and maintenance management device
CN109975745A (en) Localization method is unified in a kind of nearly far field based on reaching time-difference
CN108051792B (en) Distribution description method of scattering source coupled between target and rough surface
CN111141952A (en) Method and device for testing purity of vortex wave generated by antenna array
CN108021037B (en) Triple target array near field effect correction method
CN106997044B (en) Antenna directivity weighted factor calculation method and device in a kind of radar simulation
CN104573286A (en) Electromagnetic field simulation analysis method
WO2016077529A1 (en) Method for aligning base station antennae at a cell site
CN111695240A (en) Simulation modeling method and system for non-circular beam antenna directional pattern
Tian et al. A Structure and Circuit Coupling Modeling Method for Flexible Interconnection Points and Transmission Performance of Gold Belt in Microwave Modules
KR102408345B1 (en) Simulation system and method for verification of wind profiler

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination