不奔跑的扑翼机器人自起飞研究:初始俯仰角对起飞轨迹的影响

Terukazu Sato, Takahiro Nakano, N. Takesue
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引用次数: 2

摘要

近年来,受昆虫和鸟类行为启发的扑翼机器人已成为机器人和仿生学领域的研究热点。然而,大多数扑翼机器人需要操作员或辅助装置才能起飞。本次研究的目标是开发一种可以在不奔跑的情况下自行起飞的扑翼机器人,可以像无人机一样使用。本文介绍了为此目的研制的扑翼机器人的发展和评价。该机器人可以通过简单的扑翼机构和轻量化设计产生超过自身重量的推力。利用力传感器测得的推力和滑翔实验中估计的阻力系数对飞机的空速进行了仿真,结果表明,在扑翼开始0.3 s后,飞机的空速超过了起飞所需的最小空速。起飞实验结果表明,在初始俯仰角较大的情况下,可以实现起飞。然而,由于扑翼运动产生的俯仰力矩,在起飞后俯仰角立即减小。尾翼上的力矩不足以使机器人在起飞时以低空速保持水平姿态。由此得出结论,机器人需要一个控制机构来控制由扑翼运动产生的俯仰力矩和/或起飞时没有扑翼的加速器,如后肢。因此,估计了驱动后肢设计所需的参数。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Study on Self-Takeoff of a Flapping Robot without Running: Influence of the Initial Pitch Angle on the Takeoff Trajectory
Recently, research on flapping robots inspired by the behavior of insects and birds has become a focus of attention in the fields of robotics and biomimetics. However, most flapping robots require an operator or an assistance device to take off. The goal of this study was to develop a flapping robot that can achieve self-takeoff without running and can be used like a drone. This paper describes the development and evaluation of the flapping robot developed with this aim. The developed robot can generate a thrust that exceeds its own weight with a simple flapping mechanism and a lightweight design. The airspeed was simulated using the thrust measured with a force sensor and the resistance coefficient estimated in a gliding experiment, and it was found to exceed the minimum airspeed required to achieve takeoff 0.3 s from the onset of flapping. The result of the takeoff experiment demonstrated that takeoff was possible if the initial pitch angle was high. However, the pitch angle decreased immediately after takeoff due to the pitching moment generated by the flapping motion. The moment on the tail wing was not enough for the robot to maintain a horizontal posture at low airspeeds during takeoff. It was concluded that the robot requires a control mechanism for the pitching moment generated by the flapping motion and/or accelerators that function without flapping during takeoff, such as hind limbs. Therefore, the parameters required for the design of actuated hind limbs were estimated.
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