In this paper an IMC based design methodology for tracking of the spacecraft attitude is proposed. The plant is first stabilized using state feedback control based on Lyapunov theory. Adaptive attitude tracking is established by incorporating an IMC structure along with the feed- forward controller using the normalized least mean square adaptation algorithm. It has been shown that the output of the plant tracks the desired trajectory with a delay. Computer simulation results show the effectiveness of the proposed method.
Internal model control-based adaptive attitude tracking
Adaptive Lageregelung auf Basis eines internen Modells
Robot Motion and Control 2007, RoMoCo, International Workshop on Robot Motion and Control, 6 ; 39-48
2007
10 Seiten, 5 Bilder, 20 Quellen
Conference paper
English
Nonlinear Model Reference Adaptive Control for Satellite Attitude Tracking
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