DocumentCode :
577686
Title :
Parameter convergence analysis in adaptive disturbance rejection problem of rigid spacecraft
Author :
Chen, Zhiyong ; Huang, Jie
Author_Institution :
Sch. of Electr. Eng. & Comput. Sci., Univ. of Newcastle, Callaghan, NSW, Australia
fYear :
2012
fDate :
6-8 July 2012
Firstpage :
1418
Lastpage :
1423
Abstract :
The asymptotic rejection of rigid spacecraft systems under multi-tone sinusoidal disturbances with unknown frequencies was studied recently. It was shown that the problem can be solved via an adaptive control approach. However, the convergence issue of the estimated frequencies to the unknown frequencies has not been investigated. In this paper, we further give some sufficient conditions for guaranteeing the convergence of the estimated frequencies to the unknown frequencies.
Keywords :
adaptive control; aerospace control; attitude control; convergence; space vehicles; adaptive control; adaptive disturbance rejection problem; asymptotic rejection; attitude control; convergence issue; estimated frequencies; multitone sinusoidal disturbances; parameter convergence analysis; rigid spacecraft control; unknown frequencies; Adaptive control; Attitude control; Closed loop systems; Convergence; Frequency estimation; Space vehicles; Vectors; Nonlinear systems; adaptive control; internal model; spacecraft systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Automation (WCICA), 2012 10th World Congress on
Conference_Location :
Beijing
Print_ISBN :
978-1-4673-1397-1
Type :
conf
DOI :
10.1109/WCICA.2012.6358102
Filename :
6358102
Link To Document :
بازگشت