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Missile borne Synthetic Aperture Radar can effectively improve the guidance accuracy of the Inertial Guidance System
of long-range missile. The basic principle of the missile geo-location is described at first. According to the range
equations and Doppler equations, the analytical mathematical expressions of the missile's position are deduced without
complicated and unstable iterations, and the detailed flow of the missile position solving is described. Based on
simulation, the effects of digital image matching, altitude and velocity errors on the geo-location accuracy are compared.
Yu Liang Qin,Bin Deng,Hong Qiang Wang, andXiang Li
"Missile geo-location using missile-borne SAR", Proc. SPIE 6795, Second International Conference on Space Information Technology, 67952V (10 November 2007); https://doi.org/10.1117/12.774189
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Yu Liang Qin, Bin Deng, Hong Qiang Wang, Xiang Li, "Missile geo-location using missile-borne SAR," Proc. SPIE 6795, Second International Conference on Space Information Technology, 67952V (10 November 2007); https://doi.org/10.1117/12.774189