Full linear control of a quadrotor UAV, LQ vs H∞

O. Araar, N. Aouf
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引用次数: 41

Abstract

Quadrotors low level control has attracted the attention of many research works over the last decade. In most of previous works, position stabilisation was achieved using nonlinear control techniques. In this paper, two full linear techniques based on optimal control theory are presented. The first, based on the L2 norm, is a Linear Quadratique Servo (LQ-Servo) controller. The second one, optimizes the L∞ norm and is designed using H∞ control approach. Emphasis is placed on the robustness to external disturbances and particularly wind gusts. Simulation results based on the full nonlinear model of the quadrotor are presented as a basis of comparison between the two controllers.
四旋翼无人机的全线性控制,LQ vs H∞
近十年来,四旋翼飞行器的低电平控制引起了许多研究工作的关注。在以前的大多数工作中,位置稳定是使用非线性控制技术实现的。本文提出了两种基于最优控制理论的全线性控制方法。第一种是基于L2范数的线性二次伺服(LQ-Servo)控制器。第二,优化L∞范数,采用H∞控制方法进行设计。重点放在对外部干扰,特别是阵风的鲁棒性上。给出了基于四旋翼飞行器全非线性模型的仿真结果,作为两种控制器之间比较的基础。
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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