Position Controller for a Flapping-Wing Drone Using UWB

Guillermo N. González, G. D. Croon, D. Olejnik, M. Karásek
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引用次数: 1

Abstract

This paper proposes an integral approach for accurate ultra-wideband indoor position control of flapping-wing micro-air vehicles. Three aspects are considered to achieve a reliable and accurate position controller. The first aspect is a velocity/attitude flapping-wing model for drag compensation. The model is compared with real flight data and shown to be applicable for more than one type of flapping-wing drone. The second improvement regards a voltage-dependent thrust control. Lastly, a characterisation of ground effects in flapping-wing flight is obtained from hovering experiments. The proposed controller improves position control by a factor [Formula: see text], reaching a mean absolute error of 10[Formula: see text]cm for the position in [Formula: see text] and [Formula: see text], and 4.9[Formula: see text]cm for the position in [Formula: see text].
基于超宽带的扑翼无人机位置控制器
提出了一种扑翼微型飞行器超宽带室内位置精确控制的集成方法。从三个方面考虑实现可靠、准确的位置控制器。第一个方面是用于阻力补偿的速度/姿态扑翼模型。将该模型与实际飞行数据进行了比较,结果表明该模型适用于多种扑翼无人机。第二个改进与电压相关的推力控制有关。最后,通过悬停实验得到了扑翼飞行的地面效应特征。所提出的控制器将位置控制提高了一个因子[公式:见文],对于[公式:见文]和[公式:见文]中的位置,平均绝对误差为10[公式:见文]cm,对于[公式:见文]中的位置,平均绝对误差为4.9[公式:见文]cm。
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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