This paper addresses the computation of the required trajectory correction maneuvers (TCM) for a halo orbit space mission to compensate for the launch velocity errors introduced by inaccuracies of the launch vehicle.


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    Title :

    Halo Orbit Mission Correction Maneuvers Using Optimal Control


    Contributors:
    Lo, M. (author) / Serban, R. (author) / Petzold, L. (author) / Koon, W. (author) / Ross, S. (author) / Marsden, J. (author) / Wilson, R. (author)

    Published in:

    Publication date :

    2000-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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