Title :
Adaptive back-stepping LPV control of satellite attitude maneuvers with sum of squares
Author :
Jia, Wang ; Ming, Zeng ; Zhiwei, Yu ; Bin, Liu ; Wenguang, Xu
Author_Institution :
Space Control & Inertial Technol. Res. Center, Harbin Inst. of Technol., Harbin, China
Abstract :
The main contribution of this paper is that, to improve the performance properties of satellite attitude manoeuvre controlled by nonlinear stabilizing control law derived from standard adaptive back-stepping method, a hybrid control approach is developed to guarantee the stability of system in global sense while improving control performance of satellite attitude manoeuvre problem in a local region. This will be achieved by firstly using the adaptive back-stepping controller until the state trajectories entering a small region around the stability origin, Within the region system will be treated as an LPV system, then use LPV control method to improve the performance properties. a new computationally efficient LPV synthesis method using SOS was proposed, this method change the search for positive definite stability certificate functions to SOS certificate functions of appropriate polynomials. The effectiveness of the proposed control technique is shown in simulations.
Keywords :
adaptive control; artificial satellites; attitude control; control system synthesis; nonlinear control systems; polynomials; position control; stability; LPV synthesis method; adaptive back-stepping LPV control; nonlinear stabilizing control law; satellite attitude manoeuvre problem; stability certificate functions; sum of squares; system stability; Adaptive systems; Aerodynamics; Attitude control; Process control; Quaternions; Satellites; Stability analysis; Induced L2 norm; LPV; SOS; Satellite Attitude Maneuvers; adaptive back-stepping;
Conference_Titel :
Intelligent Control and Automation (WCICA), 2010 8th World Congress on
Conference_Location :
Jinan
Print_ISBN :
978-1-4244-6712-9
DOI :
10.1109/WCICA.2010.5554608