Design method of geostationary SAR bistatic configuration based on moving target detection
A technology of moving target detection and design method, which is applied in the direction of measuring device, radio wave measurement system, radio wave reflection/re-radiation, etc., can solve the problems of unconsidered performance and poor performance of moving target detection, and achieve the effect of extended functions
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Embodiment 1
[0058] This embodiment provides a GEO satellite SAR bistatic configuration design method based on moving target detection, please refer to figure 1 , the method mainly includes:
[0059] Step 1. Based on the parameters of the GEO satellite SAR system, the relationship between the system performance index and the configuration parameters is constructed.
[0060] Step 2. According to the relational expression in step 1, the configuration design problem is modeled as a multi-objective optimization problem, and the optimal bistatic configuration is obtained based on the third-generation non-dominated sorting evolutionary algorithm.
[0061] The key to determine the bistatic geometric configuration of the GEO satellite SAR moving target detection system is to establish the analytical relationship between the moving target detection performance and configuration parameters. Therefore, before the present invention determines the configuration parameters of the GEO satellite SAR syst...
Embodiment 2
[0099] On the basis of the first embodiment above, this embodiment provides a GEO satellite SAR bistatic configuration design device based on moving target detection. For at least some steps of the SAR bistatic configuration design method, please refer to Figure 4 , the device mainly includes the following modules:
[0100] The parameter acquisition module 41 is used to obtain the moving target detection performance index and configuration parameters of the GEO satellite SAR system; the moving target detection performance index includes the minimum detectable speed v r_MDV , the maximum unambiguous velocity v r_MUV , speed measurement accuracy and positioning accuracy σ x ; The configuration parameters include the ground projection ψ of the angle between the GEO satellite and the aircraft speed, and the incident angle θ of the first receiving channel of the aircraft R and the ground projection φ of the double base angle.
[0101] The model construction module 42 is used...
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