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    Adaptive Terminal Sliding Mode Fault-Tolerant Control of Spacecraft Based on the Left Attitude Error Function of SO(3)

    Adaptive Terminal Sliding Mode Fault-Tolerant Control of Spacecraft Based on the Left Attitude Error Function of SO(3) by Zhongzhong Zheng, Wei Shang, Zhou Liu, Yongda Guo

    Published 2023-01-01
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