Adaptive Fuzzy Control for an Uncertain Axially Moving Slung-Load Cable System of a Hovering Helicopter With Actuator Fault

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WEB OF SCIENCE

38
Citations

SCOPUS

43

초록

This study addresses adaptive fuzzy control for an axially moving slung-load cable system (AMSLCS) of a helicopter in the presence of an actuator fault, system uncertainty, and disturbances with the aid of a fuzzy logic system (FLS). The actuator fault considered is depicted by a more general faulty plant that includes an unknown actuator gain fault and a fault deviation vector. First, to compensate for system uncertainty and the fault deviation vector, a fuzzy control technique is adopted. Then, under the introduced FLS, a novel adaptive fuzzy control law is developed by employing a rigorous Lyapunov derivation. The closed-loop system of the AMSLCS is proved to be uniformly bounded even when considering the actuator fault, system uncertainty, and disturbances. Finally, a simulation is executed to expound the performance of the developed controller.

키워드

Actuators; Helicopters; Uncertainty; Fuzzy control; Fuzzy logic; Adaptive systems; Nonlinear systems; Actuator fault; adaptive fuzzy control; axially moving slung-load cable system (AMSLCS); system uncertainty; VIBRATION CONTROL; TOLERANT CONTROL
제목
Adaptive Fuzzy Control for an Uncertain Axially Moving Slung-Load Cable System of a Hovering Helicopter With Actuator Fault
저자
Ren, Yong; Zhao, Zhijia; Ahn, Choon Ki; Li, Han-Xiong
DOI
10.1109/TFUZZ.2022.3164512
발행일
2022-11
유형
Article
저널명
IEEE Transactions on Fuzzy Systems
권
30
호
11
페이지
4915 ~ 4925