Control of flexible spacecraft using nonlinear approximation of input shape dependence on reorientation maneuver parameters
World congress; 13th, Vol P; Aerospace, transportation systems ; 1996 ; San Francisco; CA
1997-01-01
6 pages
Conference paper
English
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Nonlinear Input Shaping Control of Flexible Spacecraft Reorientation Maneuver
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|Reorientation maneuver for spinning spacecraft
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