非线性控制策略改善系留无人直升机悬停性能

Luis A. Sandino, M. Béjar, K. Kondak, A. Ollero
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引用次数: 10

摘要

无人直升机的悬停能力会受到风效应的严重影响。在这种情况下,改善悬停性能的一个可能的解决方案是使用系绳装置,利用将直升机连接到地面的电缆施加的张力。本文提出了一种更详细的直升机控制策略,在这种增强设置中扩展了作者以前在该主题上的工作。特别地,将经典PID控制律与模型反演块相结合构成了新控制器的基础。此外,还考虑了抵消旋转联轴器的前馈作用。所得到的非线性控制结构较好地考虑了系留系统的复杂性和非线性特性。在人工风影响下的仿真验证了该控制器的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Improving hovering performance of tethered unmanned helicopters with nonlinear control strategies
Hovering capabilities of unmanned helicopters can be seriously affected by wind effects. One possible solution for improving hovering performance under such circumstances is the use of a tethered setup that takes advantage of the tension exerted on the cable that links the helicopter to the ground. This paper presents a more elaborated strategy for helicopter control in this augmented setup that extends previous work on the subject by the authors. Particularly, a combination of classical PID control laws together with model inversion blocks constitutes the base of the new controller. Additionally, feed-forward action for counteracting rotational couplings is also accounted for. The resulting nonlinear control structure considers the complex and nonlinear nature of the tethered system in a better way. Several demonstrating simulations under artificially generated wind influences are presented to endorse the validity of the new proposed controller.
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