控制理论(社会学)
跟踪(教育)
模糊逻辑
固定翼
控制工程
计算机科学
控制(管理)
模糊控制系统
工程类
人工智能
航空航天工程
心理学
教育学
翼
作者
Haoxiang Ma,Ruonan Ren,Fazhan Tao,Zhumu Fu,Nan Wang
标识
DOI:10.1016/j.ast.2024.109019
摘要
During the actual flight of unmanned helicopters, there are widespread output constraints, system uncertainties and external disturbances, which bring significant threats to their safe flight. To keep the output constraints from violating predefined boundaries, the barrier Lyapunov function (BLF) is utilized in this paper. The system uncertainties are estimated by the fuzzy logic system (FLS). The compound disturbances composed of the external disturbances and the approximation errors caused by FLS are approximated by the fixed-time disturbance observers (FTDOs). According to the analysis of FTDOs and fixed-time stability theory, the observer errors and state errors converge to a region of the origin in fixed-time, and the appropriate parameters of FTDOs and controller are designed to ensure that the disturbance convergence time is faster than the one of the proposed controller, which further improves the stability of the system. Moreover, the convergence time of the FTDOs FTDOs and the proposed approach only depends on the design parameters under any initial conditions with constrained outputs. The performance of the proposed control approach is verified through the simulation results.
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