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Development and Demonstration of a Flight Simulator for the Dual-Aircraft Platform Concept

机译:双飞机平台概念的飞行模拟器的开发和演示

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Dual-aircraft platform (DAP) is a novel stratospheric satellite concept that features two tethered glider-like unmanned aerial systems which exploit wind speed differential across altitudes (i.e. vertical wind shear) to literally sail without propulsion, analogous to a kite-surfer. A new simulator is developed to provide high-fidelity simulation of a simplified version of the DAP concept in which one glider-like aircraft, based on the MAXA Pro 4m airframe, is tethered to and leading a truck moving along a runway at NASA's Shuttle Landing Facility (SLF). In this paper, the components of the simulation environment are described including aircraft/cable nonlinear aerodynamic models, cable dynamics, actuator and engine models, wind and turbulence models, pilot-in-the-loop control, autonomous formation flight control, and an X-plane interface used for visualization. This simulator is used to design and evaluate novel controls strategies, including use of an unorthodox control surface configuration, and shown to enable the sailing mode of flight without propulsion.
机译:双机平台(DAP)是一种新颖的平流层卫星概念,具有两个类似滑翔机的系留无人飞行器的空中系统,该系统利用跨高空的风速差(即垂直风切变)在无推进的情况下进行航行,类似于风筝冲浪者。开发了一种新的模拟器,以提供DAP概念简化版本的高保真模拟,在该模型中,一架基于MAXA Pro 4m机身的类似滑翔机的飞机被束缚并引导着卡车沿着NASA的Shuttle Landing的跑道移动设施(SLF)。在本文中,描述了仿真环境的组成部分,包括飞机/电缆非线性空气动力学模型,电缆动力学,执行器和发动机模型,风和湍流模型,飞行员在环控制,自主编队飞行控制以及X平面接口用于可视化。该模拟器用于设计和评估新颖的控制策略,包括使用非传统的控制面配置,并且可以在没有推进力的情况下实现航行飞行模式。

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