Fixed-time convergence attitude control for a tilt trirotor unmanned aerial vehicle based on reinforcement learning

被引:8
|
作者
Xie, Tian [1 ]
Xian, Bin [1 ]
Gu, Xu [1 ,2 ]
机构
[1] Tianjin Univ, Tianjin 300072, Peoples R China
[2] Guiyang Univ, Guiyang 55005, Guizhou, Peoples R China
基金
国家重点研发计划; 中国国家自然科学基金;
关键词
Tilt trirotor UAV; Fixed-time convergence; Reinforcement learning; Modeling uncertainties; External disturbances; SLIDING MODE CONTROL; TRACKING CONTROL; QUADROTOR UAV; STABILIZATION; STABILITY; DESIGN; GUIDANCE; FLIGHT;
D O I
10.1016/j.isatra.2022.06.006
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents a new nonlinear robust attitude control strategy for the tilt trirotor unmanned aerial vehicle (UAV). Fixed-time convergence control of the UAV's attitude tracking errors under the effects of model uncertainties and unknown external disturbances is achieved by utilizing the proposed control design. Actor-critic (AC) structure based neural networks are trained only with the information of the UAV's inputs and outputs data, to handle the UAV's modeling uncertainties with bounded estimation error. Then a sliding-mode based fixed-time controller is designed to compensate the approximation error of the neural networks and the unknown external disturbances. Based on the Lyapunov stability theory, the stability analysis of the closed-loop system is presented. The performance of the presented nonlinear robust control strategy is validated through the real-time flight experiments.(c) 2022 ISA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:477 / 489
页数:13
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