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    AUTOMATICA
    2002
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    Halo orbit mission correction maneuvers using optimal control
    14 years 14 days 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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