Front squint SAR imaging method based on hypersonic aircraft at level flight section
A technology of hypersonic speed and imaging method, which is applied in the field of radar, can solve the problems of not considering the spatial variability of frequency modulation, poor imaging effect, highly complex algorithm, etc. Effect
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[0036] The present invention will be further described below in conjunction with the accompanying drawings.
[0037] refer to figure 1, the specific implementation steps of the present invention are as follows:
[0038] Step 1. Obtain radar echo data.
[0039] 1a) The synthetic aperture radar device is at the front end of the hypersonic vehicle, and the hypersonic vehicle follows the figure 2 The geometric relationship shown is to fly along the X-axis direction at the speed v, the X-axis direction is the azimuth direction, the Y-axis direction is the distance direction, and the radar beam is at a fixed forward oblique angle of view θ sq When the ground scene is irradiated, the instantaneous slant distance between the radar and the center of the scene is R(t m ;X n , R 0 ):
[0040] R ( t m ; X n , R ...
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