This chapter introduces the model and an extended Kalman filtering(EKF) method of satellite‐to‐satellite passive tracking using bearing only 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 Orbit Determination by Bearings Only
Space Electronic Reconnaissance ; 227-259
2014-04-08
33 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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