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Sliding Mode Fault Tolerant Attitude Control for Flexible Spacecraft Under Actuator Fault
Received date: 2010-12-22
Revised date: 2011-02-22
Online published: 2011-10-27
XIAO Bing, HU Qinglei, HUO Xing, MA Guangfu. Sliding Mode Fault Tolerant Attitude Control for Flexible Spacecraft Under Actuator Fault[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(10): 1869-1878. DOI: CNKI:11-1929/V.20110402.1751.003
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