Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults
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چکیده
منابع مشابه
Adaptive nonsingular fast terminal sliding mode control for electromechanical actuator
Adaptive nonsingular fast terminal sliding mode control for electromechanical actuator Hao Li a b , Lihua Dou a b & Zhong Su c a School of Automation, Beijing Institute of Technology, Beijing 100081, China b Key Laboratory of Complex System Intelligent Control and Decision (Beijing Institute of Technology), Ministry of Education, Beijing 100081, China c Key Laboratory of Modern Measurement and ...
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ژورنال
عنوان ژورنال: IEEE Access
سال: 2019
ISSN: 2169-3536
DOI: 10.1109/access.2019.2902671