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.


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    Title :

    Satellite‐to‐Satellite Passive Orbit Determination by Bearings Only


    Contributors:
    Guo, Fucheng (author) / Fan, Yun (author) / Zhou, Yiyu (author) / Zhou, Caigen (author) / Li, Qiang (author)

    Published in:

    Publication date :

    2014-04-08


    Size :

    33 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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