| Hybrid EDA-based optimal attitude control for a spacecraft in a class of control task |
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ACM/SIGEVO Summit on Genetic and Evolutionary Computation
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Proceedings of the first ACM/SIGEVO Summit on Genetic and Evolutionary Computation
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Shanghai, China
POSTER SESSION: Poster sessions
table of contents
Pages 903-906
Year of Publication: 2009
ISBN:978-1-60558-326-6
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Authors
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Xiong Luo
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School of Information Engineering, University of Science and Technology Beijing, Beijing 100083, Beijing, China
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Zengqi Sun
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Tsinghua University, Beijing 100084, Beijing, China
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Xiang Zhang
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Yangtze University, Jingzhou 434023, Jingzhou, China
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Laihong Hu
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Tsinghua University, Beijing 100084, Beijing, China
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Chao Wang
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School of Information Engineering, University of Science and Technology Beijing, Beijing 100083, Beijing, China
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Downloads (6 Weeks): 6, Downloads (12 Months): 14, Citation Count: 0
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ABSTRACT
In the practical situation, if failure of one of the actuators occurs, there exists the attitude control task of a rigid spacecraft using only two control torques supplied by momentum wheel actuators. Here, this class of control task for a rigid spacecraft is discussed. This nonlinear control problem can be converted to the nonholonomic motion planning optimization problem of a drift-free system. In order to improve the search efficiency of current optimization algorithms, the hybrid estimation of distribution algorithm (EDA) is presented by combing the idea of differential evolution strategy (DES). Then, the optimal attitude control task for the spacecraft using two momentum wheel actuators is achieved. By comparing the proposed algorithm with existing genetic algorithm and evolutionary programming, the simulation results show the accuracy and efficiency of hybrid EDA.
REFERENCES
Note: OCR errors may be found in this Reference List extracted from the full text article. ACM has opted to expose the complete List rather than only correct and linked references.
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