Optimal Tracking Control Experiments for 2-DOF Helicopter: An Open-Implementation Approach

Kenneth Vonckx, Glenn Janiak, Md. Suruz Miah
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引用次数: 2

Abstract

This paper advances the previous work done by Janiak et al., by implementing a generic optimal tracking control law for tracking the motion of a 2-DOF helicopter. While most of the 2-DOF helicopter control algorithms proposed in the literature to date are tested using computer simulations, the focus of the current work is to practically implement a leading optimal tracking control scheme for converging a 2-DOF helicopter to its desired configuration asymptotically. The contribution of the current manuscript is to generalize the implementation framework for various control strategies that can be deployed for controlling the motion of a set of 2-DOF helicopters. The optimal tracking control scheme considered in this work takes into account the measurements of pitch and yaw angles, and their angular speeds to generate actuator commands for main and tail propellers of a 2-DOF helicopter. The performance of the optimal tracking controller is demonstrated using a set experiments conducted in a laboratory setting.
二自由度直升机最优跟踪控制实验:一种开放实现方法
本文改进了Janiak等人的工作,实现了一种用于二自由度直升机运动跟踪的通用最优跟踪控制律。虽然迄今为止文献中提出的大多数2-DOF直升机控制算法都是使用计算机模拟进行测试的,但当前工作的重点是实际实现一种领先的最优跟踪控制方案,以使2-DOF直升机渐近收敛到所需的构型。当前手稿的贡献是概括了各种控制策略的实现框架,这些策略可以用于控制一组2-DOF直升机的运动。本文研究的最优跟踪控制方案考虑了俯仰角和偏航角的测量以及它们的角速度来生成二自由度直升机主螺旋桨和尾螺旋桨的致动器命令。通过在实验室环境中进行的一组实验,验证了最优跟踪控制器的性能。
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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