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Erschienen in:
2013 | OriginalPaper | Buchkapitel
Adaptive SMC for Attitude Stabilization in Presence of Actuator Saturation
verfasst von : Yuanqing Xia, Mengyin Fu
Erschienen in: Compound Control Methodology for Flight Vehicles
Verlag: Springer Berlin Heidelberg
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Attitude control and stabilization problem for rigid spacecraft systems with highly nonlinear characteristics has attracted a great deal of interest for its important application [216]-[196]. From a practical point of view, the design of efficient and low-cost attitude controllers is an important issue for aerospace industry. In general, the spacecraft motion is governed by the so-called kinematic equations and dynamic equations [262]. Actually, these mathematical descriptions are highly nonlinear and the conventional linear control techniques are not suitable for the control design.