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Spaceborne Bistatic InSAR Geolocation with Geostationary Transmitter

机译:具有对地静止发射机的星载双站InSAR地理位置

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The bistatic interferometric synthetic aperture radar (InSAR) system, with a geosynchronous earth orbit (GEO) illuminator and two low-earth-orbit (LEO) receivers, has the advantages of flexibility, lightweight receiving platform and low cost. However, its geometry of bistatic interferometry is complex, and its slant range equation is in the form of round-trip delay. The traditional three-dimensional (3D) positioning methods of InSAR with ‘one-transmitter and two-receivers' and repeat tracks are invalid. In order to solve this problem, firstly, we establish the bistatic InSAR target positioning equations. Secondly, according to the interferometric geometry, the conversion relationship between baseline vector and slant range vector is constructed. Then, we derive and present a closed-form solution of the bistatic InSAR target positioning in the form of geostationary GEO SAR orbit. Finally, the effectiveness of the proposed method is verified by simulation data.
机译:具有地球同步轨道(GEO)照明器和两个低地球轨道(LEO)接收器的双基地干涉合成孔径雷达(InSAR)系统具有灵活性,轻巧的接收平台和低成本的优点。但是,其双基地干涉仪的几何形状很复杂,其倾斜范围方程式为往返延迟形式。具有“一个发射器和两个接收器”以及重复轨迹的InSAR的传统三维(3D)定位方法无效。为了解决这个问题,首先,我们建立了双基地InSAR目标定位方程。其次,根据干涉几何学,建立基线矢量与斜距矢量之间的转换关系。然后,我们以对地静止GEO SAR轨道的形式导出并提出了双基地InSAR目标定位的封闭形式解决方案。最后,通过仿真数据验证了该方法的有效性。

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