Spacecraft Attitude Control Using Approximate Receding-Horizon Model-Error Control Synthesis
نویسندگان
چکیده
منابع مشابه
Spacecraft Attitude Control Using Approximate Receding-Horizon Model-Error Control Synthesis
Abstract Model-error control synthesis is a nonlinear robust control approach that mitigates the effects of modeling errors and disturbances on a system by providing corrections to the nominal control input directly. In this paper model-error control synthesis is applied to the spacecraft attitude control problem, where the model-error vector is computed using a receding-horizon approximation. ...
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ژورنال
عنوان ژورنال: Journal of Guidance, Control, and Dynamics
سال: 2006
ISSN: 0731-5090,1533-3884
DOI: 10.2514/1.15402