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Haowei Wen1, Xiaokui Yue1, Zheng Wang1
1National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi'an, 710072, PR China.
This study introduces an adaptive Robust Integral of the Sign of the Error (RISE) control method for precise attitude tracking, even with unknown inertia and external disturbances. This novel approach achieves global asymptotic tracking without needing exact disturbance bounds.
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