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VARIABLE STRUCTURE MODEL-FOLLOWING CONTROL OF SWITCHING ATTITUDE SYSTEM OF SPACECRAFT
Author(s): 
Pages: 19-24
Year: Issue:  1
Journal: Aerospace Control

Keyword:  Subject termsSpacecraftAdaptive controlNolinear systemAttitude control;
Abstract: A variable structure model-following odaptive controller for switching attitude system of some spacecraft is designed in this paper. The structure of the controller is simple and the robustness of a system ean be improved with the controller. After using bang-bang control, a rapid system response and zero steady-state error for constant disturbance can be obtained.
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