Several results on the reconfigurable control architecture for the formation flying of multiple spacecraft are presented. In this direction, simple control laws are combined with logic-based switching to propose a hybrid control architecture for leader reassignment, leader-following capturing, and dealing with control saturations.
Reconfigurable Control for the Formation Flying of Multiple Spacecraft
01.01.1998
Sonstige
Keine Angabe
Englisch
AIAA | 2003
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