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AUTOMATICA
2002
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AUTOMATICA 2002
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Halo orbit mission correction maneuvers using optimal control
15 years 3 months ago
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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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