Genetic-based fuzzy logic controller for satellites stabilized by reaction wheels and gravity gradient

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2007

Volumn 2, Issue , 2007, Pages 1435-1445

  Omar, Hanafy M ^a  

^a KING FAHD UNIVERSITY OF PETROLEUM AND MINERALS   (Saudi Arabia)

Author keywords

[No Author keywords available]

Indexed keywords

ELECTRIC POWER UTILIZATION; FUZZY CONTROL; FUZZY LOGIC; GENETIC ALGORITHMS;

DISTRIBUTED CONTROLLERS; FUZZY LOGIC CONTROLLER (FLC); LINKING PARAMETERS; YAW MOTIONS;

SATELLITES;

EID: 37249052766     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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3. Coello, C. "Theoretical and Numerical Constraint Handling Techniques used with Evolutionary Algorithms: A Survey of the State of the Art", Computer Methods in Applied Mechanics and Engineering, 191(11-12), 2002, 1245-1287.
4. Daley, S.; and Gill, K. F, Attitude Control Of A Spacecraft Using an Extended Self-Organizing Fuzzy Logic Controller, Proceedings of the Institution of Mechanical Engineers, Part C: Mechanical Engineering Science, v 201, n 2, 1987, p 97-106
5. Dixon I. and Szego, G., Numerical optimization of dynamic systems, North-Holland Co., 1980.
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8. Jamshidi M. and Ross, T., "Fuzzy Logic and Control, Software and hardware Applications", Printce-Hall, Inc. 1993.
9. Kittipong B, Nachol C., and Suwat K., Time optimal and time-energy optimal control of a satellite attitude using genetic algorithms, ASME International Mechanical Engineering Congress and Exposition, Nov 17-22 2002, New Orleans, LA, USA, 2002,217-224.
10. ∞ control of a gravity gradient stabilized satellite, Control Engineering Practice, 8, 2000, 975983.