DocumentCode :
2341278
Title :
Fuzzy control application to guidance control for lunar gravity-turn
Author :
Junwei, Sun ; Oji Ping Yuan ; Fengqiu, Liu
Author_Institution :
Deep Space Exploration Res. Center, Harbin Inst. of Technol., China
Volume :
9
fYear :
2005
fDate :
18-21 Aug. 2005
Firstpage :
5635
Abstract :
A fuzzy observer-based mixed parallel distributed compensation (PDC) fuzzy controller is utilized to generate guidance law for lunar gravity-turn descent. First, the Takagi-Sugeno fuzzy model is employed to approximate the probe system. Next, based on fuzzy model, a fuzzy observer-based mixed parallel distributed compensation (PDC) fuzzy controller is discussed in accordance with the definition of stability in the sense of Lyapunov. Robust stability and disturbance rejection technique are also proposed in the design of following guidance control.
Keywords :
Lyapunov methods; aerospace control; compensation; fuzzy control; linear matrix inequalities; observers; probes; robots; space vehicles; Lyapunov stability; Takagi-Sugeno fuzzy model; disturbance rejection; fuzzy control; fuzzy observer; guidance control; linear matrix inequality; lunar gravity-turn descent; mixed parallel distributed compensation controller; probe system; robust stability; Control systems; Fuzzy control; Fuzzy sets; Fuzzy systems; Gravity; Heuristic algorithms; Image sequences; Observers; Robust stability; Takagi-Sugeno model; background; difference algorithm; image sequence; texture characteristic;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Machine Learning and Cybernetics, 2005. Proceedings of 2005 International Conference on
Conference_Location :
Guangzhou, China
Print_ISBN :
0-7803-9091-1
Type :
conf
DOI :
10.1109/ICMLC.2005.1527940
Filename :
1527940
Link To Document :
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