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    AUTOMATICA
    2002
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    Halo orbit mission correction maneuvers using optimal control
    13 years 4 months ago
    Halo orbit mission correction maneuvers using optimal control
    Download  www.cds.caltech.edu
    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 b...
    Radu Serban, Wang Sang Koon, Martin W. Lo, Jerrold...
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