DocumentCode :
1993907
Title :
The attitude stabilization of hanging equilibrium of the 3D axially symmetric rigid pendulum with hierarchical sliding mode control
Author :
Zou, Kui ; Ge, Xinsheng
Author_Institution :
Autom. Sch., Beijing Inf. Sci. & Technol. Univ., Beijing, China
fYear :
2011
fDate :
16-18 Sept. 2011
Firstpage :
6142
Lastpage :
6146
Abstract :
3D rigid pendulum is an reduced model of GEO stationary spacecraft, and researches on the dynamics and control methods of it have great significance of the development for nonlinear system control theory. Being acted on by gravitational force, the 3D axially symmetric rigid pendulum rotates around a fixed point, if the angular velocity rotated around the axis of symmetry is zero, the system is referred as a spherical 2D pendulum; and if the angular velocity is a non-zero constant, the system is referred as a Lagrange top. This paper concentrates on hanging equilibrium control problem of a Lagrange top, and then we design a hierarchical sliding mode controller with sliding mode variable structure method. Simulation results show that this method is feasible and effective for the hanging equilibrium control of the 3D Rigid Pendulum.
Keywords :
angular velocity; attitude control; control system synthesis; nonlinear control systems; pendulums; space vehicles; stability; variable structure systems; 3D axially symmetric rigid pendulum; GEO stationary spacecraft; Lagrange top; angular velocity; attitude stabilization; gravitational force; hanging equilibrium control problem; hierarchical sliding mode control; nonlinear system control theory; sliding mode variable structure method; spacecraft reduced model; spherical 2D pendulum; Three dimensional displays; Lagrange top; Lyapunov stability; SD rigid pendulum; Sliding mode control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical and Control Engineering (ICECE), 2011 International Conference on
Conference_Location :
Yichang
Print_ISBN :
978-1-4244-8162-0
Type :
conf
DOI :
10.1109/ICECENG.2011.6058023
Filename :
6058023
Link To Document :
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