多旋翼飞行器编队鲁棒控制设计

Hasham Muzammil, N. Siddique, Saad Ali Masud, Muhammad Rashad, Uzair Raoof, Iftikhar Hussain, Waqas Jabbar
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引用次数: 0

摘要

在这项研究中,提出了一种多四旋翼飞行器的控制策略,包括滑模控制和比例导数(PD)控制,目标是在不确定的条件和环境中提供稳定性、鲁棒性、减少干扰和编队跟踪。该控制方法基于牛顿-欧拉方程,满足李雅普诺夫稳定性条件,采用滑模控制器设计和PD控制器设计。在满足Lyapunov稳定条件的情况下,以最小的位置误差、方向误差和距离误差实现了所设计的控制技术。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Robust Control Design of Multiple Quadrotors Formation
In this study, a control strategy is presented for multiple quadrotors, inclusive of sliding mode control and proportional derivative (PD) control, with the goal of providing stability, robustness, reduced disturbance, and formation tracking in uncertain conditions and environments. The presented control technique is based on Newton-Euler equations and satisfying Lyapunov’s stability conditions, using sliding mode controller design and PD controller design. The designed control technique was implemented, and the desired results were achieved with minimized position error, orientation error, and distance error, while adhering to Lyapunov’s stability conditions.
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CiteScore
0.70
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