Abstract This paper deals with the problems on the spacecraft motion in the Earth’s atmosphere taking into account the Earth’s atmospheric drag as well as on the extra-atmospheric part of the trajectory, where resistance is absent. An analytical solution of these problems by the method of fast expansions is proposed.


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    Title :

    Application of the fast expansion method for spacecraft trajectory calculation


    Contributors:

    Published in:

    Publication date :

    2015-04-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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