观察员(物理)
控制理论(社会学)
固定翼
跟踪(教育)
国家(计算机科学)
计算机科学
控制(管理)
国家观察员
容错
实时计算
控制工程
工程类
心理学
人工智能
分布式计算
算法
非线性系统
航空航天工程
物理
教育学
量子力学
翼
标识
DOI:10.1108/aeat-02-2024-0040
摘要
Purpose To improve the robustness of carrier-based unmanned aerial vehicle (UAV) with actuator faults attitude tracking control system, this paper aims to propose a fixed-time backstepping (FXTBSC) fault-tolerant control based on a fixed-time extended state observer. Design/methodology/approach A fixed-time extended state observer (FXTESO) is designed to estimate the total disturbance including nonlinear, coupling, actuator faults and external disturbances. The integration of backstepping control and fixed-time technology ensures fixed-time convergence. Findings The simulation results of tracking the desired attitude angle show that the anti-interference, fault tolerance and tracking accuracy of FXTBSC-FXTESO are better than the BSC-ESO control method. Originality/value Different from the traditional BSC-ESO, the convergence speed and convergence accuracy of FXTBSC-FXTESO proposed in this paper are better than conventional extended state observer. And the fixed time controller has the advantages of high tracking accuracy, fault tolerance and anti-interference ability.
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