DocumentCode :
1705106
Title :
Global stabilization of spacecraft rendezvous system subject to input saturation via gain scheduling
Author :
Wang Qian ; Zhou Bin ; Duan Guang-Ren
Author_Institution :
Center for Control Theor. & Guidance Technol., Harbin Inst. of Technol., Harbin, China
fYear :
2013
Firstpage :
1436
Lastpage :
1441
Abstract :
The problem of global stabilization of the circular orbit spacecraft rendezvous system with input saturation is studied in this paper. The rendezvous process is divided into the in-plane motion and the out-plane motion based on C-W equations with saturation nonlinearities in the actuators. By considering the advantages of the recently developed parametric Lyapunov equation based design method and the invariant sets theory, a globally stabilizing gain scheduling nonlinear controller is proposed. To apply the proposed gain scheduling approach, only a scalar nonlinear equation is required to be solved online. Numerical simulations show the effectiveness of the proposed approach.
Keywords :
Lyapunov methods; actuators; control nonlinearities; control system synthesis; nonlinear control systems; nonlinear equations; numerical analysis; scheduling; set theory; space vehicles; stability; C-W equations; actuators; circular orbit spacecraft rendezvous system; globally stabilizing gain scheduling nonlinear controller; in-plane motion; input saturation nonlinearities; invariant set theory; numerical simulations; out-plane motion; parametric Lyapunov equation-based design method; rendezvous process; scalar nonlinear equation; Acceleration; Closed loop systems; Eigenvalues and eigenfunctions; Equations; Mathematical model; Orbits; Space vehicles; Gain scheduling; Global stabilization; Parametric Lyapunov equation; Spacecraft rendezvous;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
Type :
conf
Filename :
6639653
Link To Document :
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