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On the Use of Tethered Configurations for Augmenting Hovering Stability in Small-size Autonomous Helicopters

机译:使用系留配置来增强小型自动直升机的悬停稳定性

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摘要

Helicopters are well-known by their hovering capabilities. However, the performance of this valuable feature can be seriously affected by external disturbances such as wind effects. The latter could be even more significant when dealing with small-size helicopters, which are commonly adopted as base platforms for developing unmanned aerial vehicles. Motivated by this context, this work proposes an augmented configuration for performing more stable hovering maneuvers that consists of the unmanned helicopter itself, a tether connecting the helicopter to the ground, and a device on ground adjusting the tether tension. A modeling analysis on the inherent benefits to the proposed configuration as well as the control guidelines to exploit such potentialities are presented in this paper. As a proof a concept, a first basic implementation of the control structure for the entire system is also included. Finally, several demonstrating simulations under artificially generated wind influences are presented to endorse the validity of the proposed approach.
机译:直升机以其悬停功能而闻名。但是,此重要功能的性能可能会受到外部干扰(例如风的影响)的严重影响。当与小型直升机打交道时,后者甚至更为重要。小型直升机通常被用作开发无人机的基础平台。受此背景的启发,这项工作提出了一种用于执行更稳定的悬停动作的增强配置,该配置包括无人驾驶直升机本身,将直升机连接到地面的系绳以及用于调节系绳张力的地面设备。本文介绍了对拟议配置的固有优势以及利用此类潜力的控制指南的建模分析。作为概念的证明,还包括整个系统的控制结构的第一个基本实现。最后,提出了几种在人工产生的风影响下的模拟仿真,以验证所提出方法的有效性。

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