Geometric correction method for spotlight-mode satellite SAR (synthetic aperture radar) image
A geometric correction and space-borne technology, applied in the field of image processing, can solve problems such as equation parameter mismatch, large positioning error, and processing accuracy impact, and achieve the effect of improving processing efficiency, increasing processing speed, and reducing calculation amount
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[0130] Embodiment: Taking a SAR image with a size of 4096×4096 as an example, the specific process is as follows figure 1 shown, including the following steps:
[0131] Step 1: Read in the relevant parameters and echo data, and establish a positioning equation consisting of three equations: slant distance equation, Doppler equation, and earth model equation on the basis of the geometric relationship between the satellite and the earth. The specific steps are divided into:
[0132] A. Read in geometric correction parameters, including ephemeris parameters and Doppler parameters: eccentricity e, semi-major axis a, ascending node equator Ω, perigee argument ω, orbital inclination i, periapsis time τ, deviation Navigation angle Ψ, pitch angle θ, roll angle Φ, radar irradiation center time t 0 , wavelength λ, Doppler center frequency Doppler frequency Reference slope distance R min , oblique angle φ, signal sampling rate f s , pulse repetition frequency prf, the approximate...
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