This chapter introduces the model and an extended Kalman filtering(EKF) method of satellite‐to‐satellite passive tracking using bearing and frequency under the two body model and J2 perturbation of earth oblateness model assumption. The system observability of passive orbit determination is analyzed and simulated.
Satellite‐to‐Satellite Passive Tracking Based on Angle and Frequency Information
Space Electronic Reconnaissance ; 261-309
2014-04-08
49 pages
Article/Chapter (Book)
Electronic Resource
English
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