开关拓扑下四旋翼机自适应鲁棒时变编队控制:理论与实验

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Aerospace America Pub Date : 2023-08-21 DOI:10.3390/aerospace10080735
Ziqiang Zhao, Ming Zhu, Jiazheng Qin
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引用次数: 0

摘要

本文研究了一种实用的时变四旋翼机群控制方法,该方法适用于受干扰、不确定性和开关导向拓扑的四旋翼机。提出了一种采用线速度无关位置控制器(LVIPC)和非奇异终端滑模姿态控制器(NTSMAC)的全分布式编队控制方案。采用分布式观测器消除了对线速度状态的测量,只需要局部相邻状态即可实现编队飞行。设计了一种时变非奇异终端滑模流形来抑制渐近相位,保证系统的有限时间收敛。采用自适应估计来消除对集总不确定性上界先验知识的依赖。然后证明了在该方法下所有闭环信号都是有界的。基于一个实际的室外硬件解决方案,对比实验结果验证了所提控制算法的有效性。
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Adaptive Robust Time-Varying Formation Control of Quadrotors under Switching Topologies: Theory and Experiment
This paper investigates a practical time-varying formation control method for quadrotors subjected to disturbances, uncertainties, and switching-directed topologies. A fully distributed formation control scheme is proposed using a linear-velocity independent position controller (LVIPC) and a nonsingular terminal sliding mode attitude controller (NTSMAC). A distributed observer is adopted to eliminate the measurement of linear-velocity states, and only local neighbor states are needed to realize formation flight. A time-varying nonsingular terminal sliding mode manifold is designed to suppress the reaching phase and ensure the finite-time convergence. Adaptive estimators are employed to remove the reliance on the prior knowledge of the upper bound of lumped uncertainties. It is then proven that all the closed-loop signals are bounded under the proposed method. Comparative experimental results based on a practical outdoor hardware solution are presented to confirm the effectiveness of the suggested control algorithm.
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
0.00%
发文量
9
审稿时长
4-8 weeks
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