DocumentCode
456706
Title
Adaptive Backstepping Control for Flight Simulator
Author
Wang, Qingwei ; Liu, Zhenghua ; Er, Lianjie
Author_Institution
Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut.
Volume
2
fYear
2006
fDate
Aug. 30 2006-Sept. 1 2006
Firstpage
134
Lastpage
137
Abstract
The flight simulator is a kind of servo system with uncertainties and disturbances. To obtain high performance and good robustness for the flight simulator, we present an adaptive backstepping controller, which is robust to the parameter uncertainties and load disturbances. First, the model of the flight simulator with parameter uncertainties and load torque disturbances is proposed based on experiment test. Second, the design procedure of the adaptive backstepping controller is described and analyzed. The parameter update law and control law are designed based on Lyapunov stability theorem. Simulation results clearly show that the proposed control scheme can track the position reference signal successfully under parameter uncertainties and load torque disturbance
Keywords
Lyapunov methods; adaptive control; aerospace control; aerospace simulation; control system synthesis; nonlinear control systems; position control; robust control; servomechanisms; Lyapunov stability theorem; adaptive backstepping controller design procedure; control law design; flight simulator; load torque disturbance; parameter uncertainty; parameter update law design; position reference signal tracking; servo system; Adaptive control; Aerospace simulation; Backstepping; Programmable control; Robust control; Servomechanisms; Testing; Torque; Uncertain systems; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Innovative Computing, Information and Control, 2006. ICICIC '06. First International Conference on
Conference_Location
Beijing
Print_ISBN
0-7695-2616-0
Type
conf
DOI
10.1109/ICICIC.2006.225
Filename
1691946
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