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Parameter design for a guidance and control system using genetic approach

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Keywords: genetic algorithms; guidance and control; missile; optimization; stability

Document Type: Research Article

DOI: http://dx.doi.org/10.1016/S1270-9638(01)01121-X

Affiliations: Institute of Automatic Control Engineering, Feng Chia University, 40724, Taichung, Taiwan

Publication date: September 1, 2001

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