Sliding Mode Control Design for Aircraft Control Systems
Author:
- 24 August 2005
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 309-313
Abstract
In this paper, a sliding mode controller design for the robust control of uncertain systems is developed. The method is applied to a vertical takeoff and landing aircraft whose aerodynamic parameters vary considerably during flight. The control law consists of a nominal continuous control and a switching control which numerical computation is simple. The tracking performance as well as the robustness against system parameter uncertainties is illustrated.Keywords
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