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Spacecraft Attitude Control Based on Fuzzy Variable Structure
WANG Qing;HUA Ying;DONG Chao-yang;ZHANG Ming-lian
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2006, (6): 1181 -1184 . 

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341