A nonparallel hexrotor UAV with faster response to disturbances for precision position keeping

Guangying Jiang, R. Voyles
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引用次数: 49

Abstract

This paper presents a fully actuated UAV platform with a nonparallel design. Standard multirotor UAVs equipped with a number of parallel thrusters would result in underactuation. Fighting horizontal wind would require the robot to tilt its whole body toward the direction of the wind. We propose a hexrotor UAV with nonparallel thrusters which results in faster response to disturbances for precision position keeping. A case study is presented to show that hexrotor with a nonparallel design takes less time to resist wind gust than a standard design. We also give the results of a staged peg-in-hole task that measures the rising time of exerting forces using different actuation mechanisms.
一种对扰动快速响应的非平行六旋翼无人机
提出了一种非并行设计的全驱动无人机平台。标准多旋翼无人机配备了一些平行推进器将导致驱动不足。对抗水平风需要机器人将整个身体向风的方向倾斜。提出了一种非平行推进器的六旋翼无人机,该无人机对干扰的响应速度更快,可以实现精确的位置保持。算例分析表明,非平行设计的六旋翼比标准设计的六旋翼抗阵风时间短。我们还给出了一个分段钉入孔任务的结果,该任务测量了使用不同驱动机构施加力的上升时间。
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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