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Flexible Spacecraft Attitude Robust Tracking Control Based on Fractional Order Sliding Mode
DENG Liwei, SONG Shenmin
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2013, (8): 1915 -1923 .  DOI: 10.7527/S1000-6893.2013.0173

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341