Design of robust controller based on adaptive backstepping and slide mode for flight simulator

Zhenghua Liu; Yunjie Wu; Lianjie Er

doi:10.1117/12.718057

30 October 2006 Design of robust controller based on adaptive backstepping and slide mode for flight simulator

Zhenghua Liu, Yunjie Wu, Lianjie Er

Proceedings Volume 6358, Sixth International Symposium on Instrumentation and Control Technology: Sensors, Automatic Measurement, Control, and Computer Simulation; 63583D (2006) https://doi.org/10.1117/12.718057
Event: Sixth International Symposium on Instrumentation and Control Technology, 2006, Beijing, China

Abstract

Considering unknown nonlinearities, external disturbances and parameter perturbations existing in the flight simulator, A backstepping and slide mode controller is designed for the flight simulator. Firstly, the dynamic model of the flight simulator is proposed by test. Secondly, the backstepping controller with friction parameter update law is deduced for this dynamic model. Finally, simulation results show that the output from the system can achieve asymptotic tracking of the given position reference signal and the aberration of velocity response under the control of common PID controller is overcome.

Citation Download Citation

Zhenghua Liu, Yunjie Wu, and Lianjie Er "Design of robust controller based on adaptive backstepping and slide mode for flight simulator", Proc. SPIE 6358, Sixth International Symposium on Instrumentation and Control Technology: Sensors, Automatic Measurement, Control, and Computer Simulation, 63583D (30 October 2006); https://doi.org/10.1117/12.718057

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