Multi-UAV adaptive super-twisting integral terminal sliding mode formation control

IF 1.5 Q2 ENGINEERING, MULTIDISCIPLINARY
Jun Wang and Mingmin Luo
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引用次数: 0

Abstract

This paper addresses issues such as model uncertainties, actuator failures, and gust disturbances in multi-quadrotor UAV formation flight. An adaptive super-twisting integral terminal sliding mode control method is proposed, incorporating a ‘Leader-Follower’ formation control strategy. The approach includes designing an adaptive super-twisting integral terminal sliding mode controller and a formation adaptive cooperative controller. Additionally, adaptive gains are utilized to manage the effects of actuator failures, gust disturbances, and ground station interference, ensuring safe formation flight. Simulation and experimental results indicate that the proposed controller can track the target trajectory within a finite time and effectively maintain formation flight.
多无人机自适应超扭曲积分终端滑模编队控制
本文探讨了多四旋翼无人机编队飞行中的模型不确定性、致动器故障和阵风干扰等问题。本文提出了一种自适应超扭积分末端滑模控制方法,并结合了 "领导者-跟随者 "编队控制策略。该方法包括设计一个自适应超扭曲积分终端滑模控制器和一个编队自适应协同控制器。此外,还利用自适应增益管理作动器故障、阵风干扰和地面站干扰的影响,确保编队飞行安全。仿真和实验结果表明,所提出的控制器能在有限的时间内跟踪目标轨迹,并有效地保持编队飞行。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Engineering Research Express
Engineering Research Express Engineering-Engineering (all)
CiteScore
2.20
自引率
5.90%
发文量
192
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