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Designing A Genetic-Based FLC For Fast Attitude Control Of Satellites with Reaction Wheels

Hanafy, M Designing A Genetic-Based FLC For Fast Attitude Control Of Satellites with Reaction Wheels. In: Second International Conference on Modeling, Simulation and Applied Optimization, ICMSAO-07, March 24-27, 2007, Abu-Dhabi.

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Abstract

In this paper, a systematic technique is proposed to design an optimal fuzzy logic controller (FLC) for the fast attitude control of satellites with reaction wheels. The optimization is performed by generating the rules and the distribution of membership functions of the FLC using the genetic algorithm. To get accurate pointing, long life time, and fast response for the satellite, the deviation of the satellite from its nominal position, the consumed power, and the time of deviation are included in the optimization objective function.



Item Type:Conference or Workshop Item (Paper)
Date Type:Publication
Subjects:Aerospace
Divisions:College Of Engineering Sciences > Aerospace Engineering Dept
Creators:Hanafy, M
Email:Omar
ID Code:385
Deposited By:HANAFY MOHAMMED OMAR
Deposited On:15 Mar 2008 14:51
Last Modified:12 Apr 2011 13:07

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