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Title: Halo Orbit Mission Correction Maneuvers Using Optimal Control
Authors: Lo, M.
Serban, R.
Petzold, L.
Koon, W.
Ross, S.
Marsden, J.
Wilson, R.
Issue Date: 2000
Citation: Automatica
Abstract: 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.
Appears in Collections:JPL TRS 1992+

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