Tensegrity Structure as the Control Base of a Flight Simulator

Phillip Italiano, Cody Lafountain, Kelly Cohen, S. Abdallah
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Abstract

The aircraft industry, military, and NASA mainly rely on the Stewart platform design, a fixed ground-based flight simulator, for the preliminary stages of pilot training and the testing of new aircraft. These systems are large, and expensive to maintain and repair. In this effort, we propose a Tensegrity based structural concept as the basis for a unique and effective flight simulator. Tensegrity structures are systems of tensile cables and compressive members. This structure has a high precision of control, is lightweight, and deployable. At the University of Cincinnati, preliminary Tensegrity models have been constructed to test our understanding of a dynamic nature of the system and to provide physical models to work with. Some of these models were constructed as static models in order to gain an understanding of construction methods. Another model was constructed as a dynamic model, consisting of small pulleys and cables, to simulate the basic operations of a flight simulator. Nomenclature θ = angular velocity about x-axis φ = angular velocity about y-axis ψ = angular velocity about z-axis I. Introduction HE main objective of this project was to use SIM Mechanics® to investigate the structural properties of a Tensegrity flight simulator. In order to accomplish this goal, it was necessary to develop algorithms that determine the necessary cable length variations to establish stable dynamic Tensegrity structures. These structures were then manipulated to simulate the perturbations required to accurately simulate the characteristics of an aircraft. Once the range of motion for a Tensegrity structure of this type was determined, the structures were subjected to external forces to determine the dynamic responses. This system will be dynamically controlled and respond in real time to the pilot's commands. The reasoning for this project is to design a flight simulator that could be used for micro UAV's in wind tunnels and the replacement of conventional high-energy flight simulators.
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张拉整体结构作为飞行模拟器的控制基础
飞机工业、军事和NASA主要依靠斯图尔特平台设计,这是一种固定的地面飞行模拟器,用于飞行员训练和新飞机测试的初步阶段。这些系统体积庞大,维护和维修费用昂贵。在这项工作中,我们提出了一个基于张拉整体的结构概念,作为一个独特而有效的飞行模拟器的基础。张拉整体结构是由拉伸索和压缩构件组成的系统。这种结构控制精度高,重量轻,可展开。在辛辛那提大学,初步的张拉整体模型已经建立,以测试我们对系统动态性质的理解,并提供物理模型来工作。其中一些模型被构建为静态模型,以获得对构建方法的理解。另一个模型是由小滑轮和缆绳组成的动态模型,用来模拟飞行模拟器的基本操作。术语θ =关于x轴的角速度φ =关于y轴的角速度ψ =关于z轴的角速度1介绍本项目的主要目标是使用SIM力学®来研究张拉整体飞行模拟器的结构特性。为了实现这一目标,有必要开发算法来确定必要的索长度变化,以建立稳定的动态张拉整体结构。然后操纵这些结构来模拟精确模拟飞机特性所需的扰动。一旦确定了这种类型的张拉整体结构的运动范围,结构就会受到外力来确定动力响应。该系统将被动态控制并实时响应飞行员的指令。本项目的目的是设计一种可用于风洞微型无人机的飞行模拟器,替代传统的高能飞行模拟器。
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