Spacecraft long-duration phasing maneuver optimization using hybrid approach

Before a manned orbital rendezvous mission, the target spacecraft usually performs several maneuvers to adjust the initial phase angle of the orbital rendezvous and to coordinate the injection of the chaser. This maneuvering process is referred to as the “target phasing mission”. This target phasing...

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Bibliographic Details

Published in:	Acta astronautica Vol. 72; pp. 132 - 142
Main Authors:	Zhang, Jin, Wang, Xiang, Ma, Xiao-bing, Tang, Yi, Huang, Hai-bing
Format:	Journal Article
Language:	English
Published:	Elsevier Ltd 01.03.2012
Subjects:	Hybrid optimization Long-duration maneuver planning Mixed integer nonlinear programming Orbital rendezvous Target spacecraft Orbital rendezvous Mixed integer nonlinear programming Long-duration maneuver planning Hybrid optimization Target spacecraft
ISSN:	0094-5765, 1879-2030
Online Access:	Get full text
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