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Hybrid control of backstepping incorporated with L2-gain analysis for aircraft attitude

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3 Author(s)
Zha Xu ; Harbin Inst. of Technol., China ; Hu Yunan ; Cui Pingyuan

A novel hybrid control approach of backstepping incorporated with L2-gain analysis for attitude control of aircraft systems with external disturbance and uncertainties is presented. An explicit solution to the nonlinear H attitude control problem can be obtained by combining backstepping and variable structure control techniques. The attitude controller achieves good performance, and the unknown disturbance is attenuated. Finally, nonlinear six-degree-of-freedom simulation results for the aircraft model are presented to demonstrate the effectiveness of the proposed control law.

Published in:

Intelligent Control and Automation, 2004. WCICA 2004. Fifth World Congress on  (Volume:6 )

Date of Conference:

15-19 June 2004