DocumentCode :
3041916
Title :
Fast terminal sliding mode control of harmonic drive system considering nonlinear attributes
Author :
You, Bindi ; Zhao, Yang ; Wang, Ran ; Sun, Shusen
Author_Institution :
Aerosp. Eng., Harbin Inst. of Technol., Harbin, China
fYear :
2010
fDate :
8-10 June 2010
Firstpage :
228
Lastpage :
232
Abstract :
Precision positioning performance is degraded by nonlinear effects of dynamic error and flexibility with harmonic drive systems. To compensate for dynamic error in the presence of nonlinear flexibility in high precision tracking, the nonlinear dynamic equation with dynamic error of harmonic drive is established by Lagrange method. Then, it is inverted to the state equation for control design. The nonlinear term is introduced into the design of the sliding mode based on the idea of terminal sliding mode control. Then, Fast terminal sliding mode controller is designed and the asymptotical stability of the system is guaranteed using Lyapunov method. The control scheme not only guarantees the convergence of the output tracking error in a finite time period but keeps the state of the system always at the terminal sliding surface. Simulation results show that the controller realize complete compensation of output errors with fast transient response. It is verified the feasibility of the control scheme.
Keywords :
Lyapunov methods; asymptotic stability; control system synthesis; drives; nonlinear dynamical systems; position control; transient response; variable structure systems; Lagrange method; Lyapunov method; asymptotical stability; compensation; control design; dynamic error; fast terminal sliding mode control; finite time period; harmonic drive systems; high precision tracking; nonlinear attributes; nonlinear dynamic equation; nonlinear effects; nonlinear flexibility; nonlinear term; output errors; output tracking error; precision positioning performance; sliding mode design; state equation; terminal sliding surface; transient response; Equations; Gears; Harmonic analysis; Mathematical model; Nonlinear dynamical systems; Sliding mode control; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
Type :
conf
DOI :
10.1109/ISSCAA.2010.5633075
Filename :
5633075
Link To Document :
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