The problem of designing suitable discrete-time attitude controllers for magnetically actuatedspacecraft is considered. A number of different techniques is considered and a novel approach tothe tuning of "projection based" controllers based on periodic optimal control is proposed. Theadvantages of the proposed method are presented, discussed, and validated in a simulation study.
Optimal discrete-time magnetic attitude control of satellites
2005 ; Prague (Czech Republic)
2005-03-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
OPTIMAL DISCRETE-TIME DESIGN OF MAGNETIC ATTITUDE CONTROL LAWS
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