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Super-Maneuver Flight control design using constrained adaptive backstepping and sliding mode

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5 Author(s)
Qin Shuo ; Aviation Theor. Dept., Air-force Aviation Univ., ChangChun, China ; Li You-Yi ; Yang Jun ; Xie Xin-Yue
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Super-maneuver flight control is designed based on constrained backstepping and second-order sliding mode. A sort of MIMO second order sliding mode algorithm is designed. The main advantages of the Super-Maneuver flight control law combined backstepping and second order sliding mode are the prevention of chattering, higher accuracy and a significant simplification of the control law. The results of super-maneuver flight simulation show that the system achieves high dynamic and static performance and robustness.

Published in:

Control Conference (CCC), 2010 29th Chinese

Date of Conference:

29-31 July 2010

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