Optimization of Satellite Momentum Wheel Control System Based on Genetic Programming

Yu Song Huang; Yun Feng Dong

doi:10.4028/www.scientific.net/AMR.748.771

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 748Optimization of Satellite Momentum Wheel Control...

Optimization of Satellite Momentum Wheel Control System Based on Genetic Programming

Abstract:

Due to reliability requirements, the reaction wheel actuator of the satellite attitude control system always use traditional control method. For the satellite which has complex structure, it's difficult to build the mathematical model with classical control method. The selection of control parameters is also difficult. The design process last long and the model have poor adaptability when the parameters change. Compare to genetic algorithms, genetic programming which have the capabilities to evolve automatically, have the advantage of being able to optimize the structure of the mathematical model. Results of optimization and simulation show that design the reaction wheel actuator control law with genetic programming can simplify the design process. And the evolved control law is better than traditional PD control law.

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Periodical:

Advanced Materials Research (Volume 748)

Pages:

771-778

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.748.771

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Online since:

August 2013

Authors:

Yu Song Huang, Yun Feng Dong

Keywords:

Control Law, Dynamic, Genetic Programming, Optimization, Satellite Attitude Control

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