DocumentCode
424154
Title
Low thrust fuzzy control in relative motion and comparison with classical methods
Author
Wang, Shi ; Dai, Jin-Hai ; Chen, Zhong ; Xu, Xin
Author_Institution
Sch. of Aerosp. & Mater. Sci., Nat. Univ. of Defense Technol., Changsha, China
Volume
3
fYear
2004
fDate
26-29 Aug. 2004
Firstpage
1947
Abstract
This paper discusses how to design fuzzy controllers of chasing spacecraft in relative motion. Fuzzy controllers are designed to apply to fuzzy logic, and simulation results illustrate the feasibility of the controllers. Furthermore, fuzzy control method and classical methods are compared with each other and the results show that fuzzy controllers have robustness.
Keywords
control system synthesis; fuzzy control; fuzzy logic; mathematical analysis; motion control; optimal control; space vehicles; chasing spacecraft; fuzzy controller design; fuzzy logic; low thrust fuzzy control; mathematical analysis; optimal control; relative motion; robustness; Aerospace engineering; Equations; Fuzzy control; Fuzzy logic; Materials science and technology; Mathematical model; Motion control; Space technology; Space vehicles; Target tracking;
fLanguage
English
Publisher
ieee
Conference_Titel
Machine Learning and Cybernetics, 2004. Proceedings of 2004 International Conference on
Print_ISBN
0-7803-8403-2
Type
conf
DOI
10.1109/ICMLC.2004.1382098
Filename
1382098
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