利用腱鞘机制进行柔性膜翼翘曲

Shian Lee, T. Tjahjowidodo, S. K. Moon
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引用次数: 6

摘要

柔性膜翼有许多优点,但其滚转控制能力很小。在本文中,柔性膜翼是由一个肌腱鞘机构驱动,以实现滚转控制,也允许机翼折叠。本文讨论了柔性机翼的特点,以及柔性机翼翘曲驱动方法。给出了实验装置和实验结果。肌腱鞘的特性适合于柔性翼的驱动。提出了一种简单的非线性曲线拟合模型。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Flexible membrane wing warping using tendon-sheath mechanism
Flexible membrane wings have many advantages, but has very little roll control authority. In this paper, the flexible membrane wing is actuated using a tendon-sheath mechanism to achieve roll control and also allowing the wing to fold. The characteristics of the flexible wing, as well as the wing warping actuation approach is discussed in this paper. The experimental setup and results are shown. The characteristics of the tendon-sheath is shown to be suitable for flexible wing actuation. A simple nonlinear curve fitting model is also presented.
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