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Design and control of tensegrity morphing airfoils

机译:变形变形翼型的设计与控制

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摘要

We present a general approach of design, dynamics, and control for tensegrity morphing airfoils. Firstly, based on reduced order Class-k tensegrity dynamics, a shape control law for tensegrity systems is derived. Then, we develop a method for discretizing continuous airfoil curves based on shape accuracy. This method is compared with conventional methods (i.e. evenly spacing and cosine spacing methods). A tensegrity topology for shape controllable airfoil is proposed. A morphing tensegrity airfoil example is given to demonstrate successful shape control. This work paves a road towards integrating structure and control design, the principles developed here can also be used for 3D morphing airfoil design and control of various kinds of tensegrity structures. Published by Elsevier Ltd.
机译:我们提出了一种设计,动态和控制的一般方法,用于变形的翼型。 首先,基于减少的顺序-K TenseGrity动态,推导了一种TenseGrity系统的形状控制法。 然后,我们开发一种用于基于形状精度离散连续翼型曲线的方法。 将该方法与常规方法进行比较(即均匀间隔和余弦间距方法)。 提出了一种形状可控翼型的强度拓扑。 给出了变形的动态翼型示例,以证明成功的形状控制。 这项工作铺设了一条朝向整合结构和控制设计的道路,这里开发的原理也可用于3D变形翼型设计和控制各种静态结构。 elsevier有限公司出版

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