DocumentCode
2276490
Title
Fuzzy logic attitude control for Cassini spacecraft
Author
Chiang, Richard Y. ; Jang, Jyh-Shing Roger
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
1994
fDate
26-29 Jun 1994
Firstpage
1532
Abstract
A fuzzy logic attitude controller has been developed for Cassini spacecraft. Feedback control issues such as tracking capability, thruster on/off time and cycle have been investigated and compared with conventional bang/bang control. A discrete nonlinear simulation was set up to assess the system performance with different controllers
Keywords
aerospace control; attitude control; feedback; fuzzy control; fuzzy logic; space vehicles; Cassini spacecraft; attitude control; discrete nonlinear simulation; feedback control; fuzzy logic control; system performance; thruster on/off time; tracking; Aircraft manufacture; Attitude control; Fuzzy logic; Laboratories; Motion control; Propulsion; Relays; Saturn; Space vehicles; Torque;
fLanguage
English
Publisher
ieee
Conference_Titel
Fuzzy Systems, 1994. IEEE World Congress on Computational Intelligence., Proceedings of the Third IEEE Conference on
Conference_Location
Orlando, FL
Print_ISBN
0-7803-1896-X
Type
conf
DOI
10.1109/FUZZY.1994.343922
Filename
343922
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