Radar precision analysis method based on distance alignment

A technology of precision analysis and radar, which is applied in the field of radar, can solve problems such as precision analysis result errors, achieve the effect of eliminating time errors and improving accuracy

Active Publication Date: 2020-05-29
成都汇蓉国科微系统技术有限公司
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AI Technical Summary

Problems solved by technology

The existing radar accuracy analysis method is to fly a designated aircraft, carry GPS information on the aircraft, and then compare and analyze the various accuracy of the radar after time alignment of the aircraft track obtained by GPS and the target track information obtained by radar. There is a problem that is easy to be ignored in the above

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  • Radar precision analysis method based on distance alignment
  • Radar precision analysis method based on distance alignment
  • Radar precision analysis method based on distance alignment

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Embodiment Construction

[0039] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is only some embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0040] A radar accuracy analysis method based on distance alignment provided by the present invention will be described in more detail below with reference to the accompanying drawings and embodiments.

[0041] Such as figure 1 As shown, the radar accuracy analysis method based on distance alignment includes:

[0042] 10. The aircraft is eq...

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Abstract

The invention provides a radar precision analysis method based on distance alignment, and the method comprises the steps: allowing an aircraft to carry positioning and navigation equipment and fly back and forth at a constant speed, and obtaining the target trace point information of the aircraft by a radar; obtaining flight path information of the aircraft by the radar and obtaining flight path information recorded by the positioning and navigation equipment carried by the aircraft; converting a radar base station and the flight path information of the aircraft into a station center coordinate system taking the radar as a circle center; compensating the aircraft flight path information data obtained by the radar and the aircraft fight path information data obtained by the positioning andnavigation equipment; and comparing the compensated aircraft flight path information data measured and calculated by the radar with aircraft real flight path information data, solving an error value measured and calculated by the radar, and obtaining radar echo calculation flight path information accurate data by solving a mean value of errors and a variance. Time errors caused by echo time delayand system time delay can be effectively eliminated, and the purpose of improving the radar precision analysis precision is achieved.

Description

technical field [0001] The invention belongs to the technical field of radar, in particular to a radar precision analysis method based on distance alignment. Background technique [0002] Before the pulse Doppler radar completes the factory inspection, it is often necessary to conduct qualitative and quantitative tests on the performance of the radar to evaluate whether the radar performance meets the specified requirements. Generally, an important indicator for pulse Doppler radar performance evaluation is radar The level of distance accuracy and angular accuracy. The existing radar accuracy analysis method is to fly a designated aircraft, carry GPS information on the aircraft, and then compare and analyze the various accuracy of the radar after time alignment of the aircraft track obtained by GPS and the target track information obtained by radar. There is a problem that is easy to be ignored in the above analysis method, that is, when the track information is time-calibr...

Claims

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Application Information

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IPC IPC(8): G01S7/40
CPCG01S7/40
Inventor 鲁瑞莲杨为华金敏汪宗福孙南费德介
Owner 成都汇蓉国科微系统技术有限公司
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