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Robust Nonlinear Control System Design for Folding-wing Aerial Vehicles During Launching Time
CAO Lijia, ZHANG Shengxiu, LI Xiaofeng, LIU Yinan
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2011, (10): 1879 -1887 . 

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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