This chapter shows the equations used in the JPL computer program ASAP that are specific to the modeling of the central body disturbing function, the third-body disturbing function, as well as the equations of motion due to atmospheric drag. These descriptions are taken directly from Reference [1] by Kwok.


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    Title :

    The Mathematical Models of the Jet Propulsion Laboratory (JPL) Artificial Satellite Analysis Program (ASAP)


    Additional title:

    Space Technology Library


    Contributors:


    Publication date :

    2021-04-13


    Size :

    5 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





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