Visual-Inertial State-Estimation Using Ground Station for UAV

A. Khan, Hameed Ullah, U. Faisal, N. Mazhar, Muhammad Yusuf Khan
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Abstract

This paper presents the controller design and visual-inertial state estimation using IMU and camera for the quadrotor's flight. To accomplish this, first, the mathematical modeling of the quadrotor is presented based on Newtonian mechanics. Then a controller is designed that ensures the autonomous flight of the quadrotor. To achieve a high-level practical autonomy, state estimation is the first step. In this regard, vision-only estimation topologies are conventionally used. However, in a few very recent studies visual-inertial combined state estimation methodologies are introduced. In this research, the monocular visual-inertial system (VINS-mono) is utilized to achieve the autonomy of the quadrotor. The approach to employ this algorithm is different from existing work as the authors used offline ground computations that simplify the implementation. The results are presented to solidify the utility of the proposed method.
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基于地面站的无人机视觉惯性状态估计
本文介绍了四旋翼飞行器的控制器设计和基于IMU和相机的视觉惯性状态估计。为此,首先基于牛顿力学建立了四旋翼飞行器的数学模型。在此基础上,设计了保证四旋翼飞行器自主飞行的控制器。为了实现高水平的实际自治,状态估计是第一步。在这方面,通常只使用视觉估计拓扑。然而,在最近的一些研究中,引入了视觉-惯性组合状态估计方法。在本研究中,利用单目视觉惯性系统(VINS-mono)来实现四旋翼飞行器的自主性。采用该算法的方法不同于现有的工作,因为作者使用了简化实现的离线地面计算。实验结果验证了所提方法的实用性。
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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