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
Link To Document :
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