基于室内局部定位系统的四旋翼无人机实验建模

M. S. Arifin, Y. Y. Nazaruddin, T. Tamba, R. A. Santosa, A. Widyotriatmo
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引用次数: 3

摘要

本文报道了垂直起降型无人机(UAV)的实验建模结果。所考虑的无人机是一种无人机四旋翼无人机,它由具有四个臂的刚体组成,每个臂都安装有一个用于运动和飞行控制的转子。为了补充机载传感器(即超声传感器和IMU),实验中使用室内局部定位系统来获取四旋翼无人机的全球定位数据。建模使用系统识别技术执行,其中无人机受到某些输入并且其实时输出被观察,然后用于估计模型。实验结果表明,所建立的五阶线性状态空间方程模型能够很好地描述所考虑的四旋翼无人机的动力学特性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental Modeling of a Quadrotor UAV Using an Indoor Local Positioning System
This paper reports the results obtained from an experimental modeling of a vertical take-off and landing type unmanned aerial vehicle (UAV). The considered UAV is an ar.drone quadrotor UAV which consists of a rigid body with fours arms, each of which is mounted with a rotor for motion and flight control. To complement onboard sensors installed on the UAV (i.e. ultrasonic sensor & IMU), an indoor local positioning system is used in the experiment to obtain the global positioning data of the quadrotor UAV. The modeling is performed using system identification technique whereby the UAV is subjected to certain inputs and its real-time output is observed and then used to estimate the model. From the experiment, it was found that a fifth order linear state space equation model captures the dynamics of the considered quadrotor UAV sufficiently good.
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