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Sliding Mode Fault Tolerant Attitude Control for Flexible Spacecraft Under Actuator Fault
XIAO Bing, HU Qinglei, HUO Xing, MA Guangfu
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2011, (10): 1869 -1878 . 

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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