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Mathematical Modelling and Identification of a Quadrotor

International Conference on Computational Science and Its Applications (ICCSA)

Universidad Manuela Beltrán | Departamento de Ingeniería Mecánica y Mecatrónica | Universidad de la Costa | Departamento de Física

Cited 2|Views7
Abstract
Motivated by the important growth of VTOL vehicles research such as quadrotors and to a small extent autonomous flight, a quadrotor dynamical model is presented in this work. The purpose of this study is to get a better understanding of its flight dynamics. It is an underactuated system. So, a simplified and clear model is needed to implement controllers on these kind of unmanned aerial systems. In addition, a computational tool is used for validation purposes. For future works embedded or intelligent control systems can be developed to control them. Gyroscopic and some aerodynamics effects are neglected.
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Quadrotor,VTOL,Flight dynamics,UAV
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要点】:本文提出了一种四旋翼飞行器的数学模型,旨在深入理解其飞行动力学特性,并为开发嵌入式或智能控制系统提供理论基础。

方法】:作者通过简化模型并忽略陀螺效应和部分气动效应,建立了一个适用于无人飞行控制系统设计的四旋翼动力学模型。

实验】:文中未详细描述具体实验过程,但提到使用了计算工具进行模型验证,数据集名称未提及。