DocumentCode
3238975
Title
Flight simulator servo system friction compensation based on variable structure control
Author
Liang-yu, Su ; Wu, Wang
Author_Institution
Sch. of Electr. & Inf. Eng., Xuchang Univ., Xuchang, China
fYear
2011
fDate
27-29 May 2011
Firstpage
645
Lastpage
648
Abstract
As friction is the main nonlinear resistance in the flight simulator servo system which can lead to overall flight simulator performance degradation. The mathematical model of flight simulator servo system was created based on a three-axis servo system and the LuGre friction model was analyzed. Exponential approach law was introduced into variable structure control and the robust controller was realized. The simulation result shows the sliding mode controller has superior position tracking and speed tracking performance for low speed servo system with friction compensated effectively.
Keywords
aerospace control; aerospace simulation; compensation; friction; nonlinear control systems; position control; robust control; servomechanisms; variable structure systems; velocity control; LuGre friction model; flight simulator performance degradation; flight simulator servo system friction compensation; mathematical model; nonlinear resistance; position tracking; robust controller; sliding mode controller; speed tracking; three-axis servo system; variable structure control; Friction; Inductance; Servomotors; flight simulator servo system; friction model; simulation; variable structure control;
fLanguage
English
Publisher
ieee
Conference_Titel
Communication Software and Networks (ICCSN), 2011 IEEE 3rd International Conference on
Conference_Location
Xi´an
Print_ISBN
978-1-61284-485-5
Type
conf
DOI
10.1109/ICCSN.2011.6014652
Filename
6014652
Link To Document