Optimal reorientation of asymmetric underactuated spacecraft using differential flatness and receding horizon control
Advances in space research ; 55 , 1
2015
Aufsatz (Zeitschrift)
Englisch
Feasible Trajectory Generation for Underactuated Spacecraft Using Differential Flatness (AAS 99-323)
British Library Conference Proceedings | 2000
|Real-time trajectory optimization of an underactuated rigid spacecraft using differential flatness
Online Contents | 2012
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