Beam position design method of inclined geosynchronous orbit synthetic aperture radar
A technology of synthetic aperture radar and geosynchronous orbit, which is applied in radio wave measurement system, radio wave reflection/re-radiation, utilization of re-radiation, etc. It can solve problems such as large orbital height, long coherent accumulation time, and large distance migration
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[0064] The method of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.
[0065] In this embodiment, the satellite operates on an inclined geosynchronous orbit (IGSO) with a small eccentricity, and the average orbit parameters are as follows:
[0066] Orbit semi-major axis a: 42164.17km
[0067] orbital inclination α i : 53 degrees
[0068] Eccentricity e: 0.07
[0069] Argument of perigee ω: 270°
[0070] Antenna size: 24m in diameter
[0071] Frequency band: L band
[0072] Satellite position: equator (latitude angle α=0°)
[0073] Pulse width T p : 1ms
[0074] Guard band time T g : 10us
[0075] Resolution ρ ed : 20m
[0076] Mapping width: 400km
[0077] Range blur ratio RASR: <-20dB
[0078] Equivalent noise backscatter coefficient NESZ: <-20dB
[0079] Adopt the wave position design method of a kind of inclined geosynchronous orbit synthetic aperture radar of the present invention...
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