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Anti-unwinding attitude control of spacecraft considering input saturation and angular velocity constraint
HU Qinglei, LI Li
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2015, (4): 1259 -1266 .  DOI: 10.7527/S1000-6893.2014.0114

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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