四旋翼飞行器的次优控制

Q4 Engineering
Wesam M. Jasim, Dongbing Gu
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引用次数: 0

摘要

本文研究了四旋翼飞行器的leader-follower编队控制问题。考虑外部干扰的四旋翼动力学模型采用单位四元数表示。引入了非线性H∞设计方法,并根据一般非线性仿射系统的结果,通过求解Hamilton-Jacobi不等式,导出了领导者和随从机器人的鲁棒控制器。然后通过选取适当的参数化李雅普诺夫函数,得到了所提控制器的鲁棒性条件。所得到的状态反馈控制器建立了闭环非线性系统的渐近稳定性。此外,对于leader-follower群体控制问题,还推导了积分反演(IB)控制器。设计IB控制器的目的是通过比较来评估H∞控制器的鲁棒性。比较了两种控制器的仿真结果,证明了H∞控制器相对于IB控制器的鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Leader-Follower Formation Suboptimal Control for Quadrotors
In this work, a leader-follower formation control problem of quadrotors is investigated. The quadrotor dynamic model is represented by unit quaternion with the consideration of external disturbance. Nonlinear H∞ design approach is introduced and robust controllers for both leader and follower robots are derived by solving a Hamilton-Jacobi inequality following from a result for general nonlinear affine systems. Then some robustness conditions of the proposed controllers are obtained by selecting appropriate parametrised Lyapunov functions. The resultant state feedback controllers establish the asymptotically stability of the closed-loop nonlinear system. In addition, integral backstepping (IB) controllers are also derived for the leader-follower formation control problem. The purpose of designing IB controllers is to evaluate the robustness of H∞ controllers by comparison. The simulation results from both types of controllers are compared and robustness performance of the H∞ controllers over the IB controllers are demonstrated.
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来源期刊
International Journal of Systems, Control and Communications
International Journal of Systems, Control and Communications Engineering-Control and Systems Engineering
CiteScore
1.50
自引率
0.00%
发文量
26
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