The attitude control problem for a rigid spacecraft with highly nonlinear characteristics in three dimensions has already been extensively studied (see, e.g., [298, 130, 239, 290, 283, 196, 140] and references therein). From a practical point of view, the design of efficient and low-cost attitude controllers is an important issue for aerospace industry. Indeed, a large variety of nonlinear control schemes, using the quaternion and angular velocity in the feedback, have been proposed recently. For instance, in [261], the attitude tracking control problem for an uncertain rigid spacecraft without angular velocity measurements is addressed.
SMC for Attitude Tracking of Rigid Spacecraft with Disturbances
Lect.Notes Control
01.01.2013
37 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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