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Proceedings Paper

Design of robust controller based on adaptive backstepping and slide mode for flight simulator
Author(s): Zhenghua Liu; Yunjie Wu; Lianjie Er
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Paper 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.

Paper Details

Date Published: 30 October 2006
PDF: 5 pages
Proc. SPIE 6358, Sixth International Symposium on Instrumentation and Control Technology: Sensors, Automatic Measurement, Control, and Computer Simulation, 63583D (30 October 2006); doi: 10.1117/12.718057
Show Author Affiliations
Zhenghua Liu, Beijing Univ. of Aeronautics and Astronautics (China)
Yunjie Wu, Beijing Univ. of Aeronautics and Astronautics (China)
Lianjie Er, Beijing Univ. of Aeronautics and Astronautics (China)


Published in SPIE Proceedings Vol. 6358:
Sixth International Symposium on Instrumentation and Control Technology: Sensors, Automatic Measurement, Control, and Computer Simulation
Jiancheng Fang; Zhongyu Wang, Editor(s)

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