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Author Lin Zhao ♦ Yingmin Jia ♦ Matsuno, F.
Sponsorship IEEE Control Syst. Soc.
Source IEEE Xplore Digital Library
Content type Text
Publisher Institute of Electrical and Electronics Engineers, Inc. (IEEE)
File Format PDF
Copyright Year ©2013
Language English
Subject Domain (in DDC) Technology ♦ Engineering & allied operations ♦ Other branches of engineering
Subject Keyword Orbits ♦ Space vehicles ♦ RNA
Abstract In this paper, two types optimal adaptive time-varying sliding mode control (ATVSMC) for a class of spacecraft rendezvous systems are proposed. The sliding surfaces pass through the initial point of system at the beginning and then move towards the origin of the error state space. By designing the ATVSMC law, the reaching phase is eliminated, and the system's robustness to unknown bounded parameter uncertainties and external disturbances is guaranteed from the beginning. The existence of global siding mode is proved by Lyapunov method. Furthermore, the parameters of sliding surfaces are obtained by minimizing the integral of the infinite norm of relative position tracking error. An example is included to illustrate the obtained results.
Description Author affiliation: Dept. of Syst. & Control, Beihang Univ. (BUAA), Beijing, China (Lin Zhao; Yingmin Jia) || Dept. of Mech. Eng. & Sci., Kyoto Univ., Kyoto, Japan (Matsuno, F.)
ISBN 9781467357142
ISSN 07431546
Educational Role Student ♦ Teacher
Age Range above 22 year
Educational Use Research ♦ Reading
Education Level UG and PG
Learning Resource Type Article
Publisher Date 2013-12-10
Publisher Place Italy
Rights Holder Institute of Electrical and Electronics Engineers, Inc. (IEEE)
e-ISBN 9781467357173
Size (in Bytes) 1.17 MB
Page Count 6
Starting Page 5504
Ending Page 5509

Source: IEEE Xplore Digital Library