GEO SAR double-satellite formation configuration design method for coherence tomography
A technology of coherent tomography and design method, which is applied in the direction of using re-radiation, radio wave reflection/re-radiation, measuring devices, etc., can solve the problem that the specified interval change of the vertical baseline cannot be realized, and achieve the goal of improving performance and improving the correlation coefficient Effect
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[0033] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below through specific embodiments in conjunction with the accompanying drawings. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.
[0034] The satellite's orbital elements include semi-major axis, eccentricity, inclination, right ascension of ascending node, argument of perigee, and true anomaly, where the true anomaly can be replaced by the mean anomaly. These six orbital elements determine the unique state of the satellite. In the present invention, the user inputs the orbital elements of the main star (semi-major axis a c , eccentricity e c , inclination i c , right ascension of ascending node Ω c , Argument of perigee ω c , mean anomaly angle M c), heightwise sampling interval ΔB, heightwise initial inter...
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