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Design, Analysis and Testing of a Smart Fin

机译:智能鳍的设计,分析和测试

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摘要

The paper presents a design concept for a control fin usually used in airborne vehicles such as UAV's, Micro UAV's and missiles. The research presents the design of a smart fin with integral piezoelectric actuators embedded in the airfoil skin. Electric field applied to the actuators would twist the airfoil leading to a change of the angle of attack. The study presents, analyze and demonstrates various lamination and actuation methods including a parametric performance investigation by finite elements models and closed form analytical model. The design and the theoretical results are verified by a manufactured smart wing demonstrator subjected to series of static and dynamic lab tests.
机译:本文提出了一种通常用于诸如UAV,微型UAV和导弹等机载车辆的控制鳍的设计概念。该研究提出了一种智能翅片的设计,该翅片在机翼表皮中嵌入了集成压电致动器。施加在执行器上的电场会使机翼扭曲,导致迎角发生变化。该研究提出,分析和证明了各种层压和驱动方法,包括通过有限元模型和闭合形式分析模型进行参数性能研究。设计和理论结果由制造的智能机翼演示器进行了一系列静态和动态实验室测试验证。

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