Fixed-time fault-tolerant attitude tracking control for UAV based on fixed-time extended state observer

被引:2
|
作者
Wu, Qilong [1 ]
Zhu, Qidan [1 ]
机构
[1] Harbin Engn Univ, Coll Intelligent Syst Sci & Engn, Harbin, Peoples R China
来源
基金
中国国家自然科学基金;
关键词
Carrier-based unmanned aerial vehicle; Attitude control; Fixed-time extended state observer; Fixed-time backstepping control; SLIDING MODE CONTROL; CONSENSUS TRACKING; SPACECRAFT;
D O I
10.1108/AEAT-02-2024-0040
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
PurposeTo 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/approachA 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.FindingsThe 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/valueDifferent 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.
引用
收藏
页码:838 / 844
页数:7
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