Thrust sensor based nonlinear motor control for quadcopters

Steven T. Elliott, T. Carr
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Abstract

Multicopter unmanned aerial vehicles (UAVs) have enormous potential for many promising applications, and improvements in controls for these flying robots could have a significant impact on their efficacy. This paper describes the novel design of a nonlinear motor controller for quadcopters that uniquely incorporates thrust feedback with an onboard force sensor installed on the motor mount. This paper explains the advanced control mathematics used to derive the controller and uses Lyapunov stability analysis to prove the design is globally asymptotically stable. In addition, this work includes a simulation in MATLAB/Simulink and laboratory experiments which illustrate the design's stable and precise thrust setpoint tracking.
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基于推力传感器的四轴飞行器非线性电机控制
多旋翼无人机(uav)在许多有前途的应用中具有巨大的潜力,并且这些飞行机器人的控制改进可能对其效能产生重大影响。本文介绍了一种新颖的四轴飞行器非线性电机控制器的设计,该控制器独特地将推力反馈与安装在电机支架上的板载力传感器相结合。本文解释了用于导出控制器的高级控制数学,并利用李雅普诺夫稳定性分析证明了该设计是全局渐近稳定的。此外,本工作还包括MATLAB/Simulink仿真和实验室实验,证明了设计的推力设定值跟踪稳定精确。
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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