Flexible Launch Vehicle Attitude Control Design Using Coevolutionary Algorithm

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Publisher
IFAC
Issue Date
2004-06-01
Language
ENG
Citation

16th IFAC Symposium on Automatic Control in Aerospace

URI
http://hdl.handle.net/10203/16619
Appears in Collection
AE-Conference Papers(학술회의논문)AE-Conference Papers(학술회의논문)

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