旋翼无人机h形鲁棒控制

Alejandro Morfin-Santana, Filiberto Muñoz Palacios, I. González-Hernández, E. S. E. Quesada, S. Salazar
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引用次数: 2

摘要

本文提出了一种构型的旋翼无人机在h配置,提供了一些优于传统的多旋翼设计。采用欧拉-拉格朗日形式建立了该飞行器的数学模型。设计了一个由比例导数项和鲁棒补偿器组成的鲁棒控制器,用于跟踪参考信号。为了验证飞行器及其控制策略的有效性,给出了一组实时实验结果。
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Robust control for octorotor Unmanned Aerial Vehicle in H-Configuration
This manuscript presents a configuration for a octorotor unmanned aerial vehicle in H-configuration that offers some advantages over traditional multirotor designs. The mathematical model for the vehicle is developed using Euler-Lagrange formalism. A robust controller, formed by a proportional derivative term and a robust compensator, is designed to track a reference signal. To show the effectiveness of the aerial vehicle and the control strategy developed, a set of real-time experimental results are presented.
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