This chapter introduces geolocation of emitter of earth by a single satellite by kinematic parameters which include frequency, frequency changing rate, time of arrival(TOA), interferometer phase rate of changing information. The geolocation error is simulated and the Cramer‐Rao lower bound(CRLB) of geolocation error is also analyzed.
Single‐Satellite Geolocation System Based on the Kinematic Principle
Space Electronic Reconnaissance ; 177-201
2014-04-08
25 pages
Article/Chapter (Book)
Electronic Resource
English
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