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首页> 外文会议>AIAA Guidance, Navigation and Control Conference Pt.2, Aug 1-3, 1994, Scottsdale, AZ >PILOTED EVALUATION OF AN INTEGRATED METHODOLOGY FOR PROPULSION AND AIRFRAME CONTROL DESIGN
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PILOTED EVALUATION OF AN INTEGRATED METHODOLOGY FOR PROPULSION AND AIRFRAME CONTROL DESIGN

机译：推进和飞机控制设计综合方法的图形化评估

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摘要

An integrated methodology for propulsion and airframe control has been developed and evaluated for a Short Take-Off Vertical Landing (STOVL) aircraft using a fixed base flight simulator at NASA Lewis Research Center. For this evaluation the flight simulator is configured for transition flight using a STOVL aircraft model, a full nonlinear turbofan engine model, simulated cockpit and displays, and pilot effectors. The paper provides a brief description of the simulation models, the flight simulation environment, the displays and symbology, the integrated control design, and the piloted tasks used for control design evaluation. In the simulation, the pilots successfully completed typical transition phase tasks such as combined constant deceleration with flight path tracking, and constant acceleration wave-off maneuvers. The pilot comments of the integrated system performance and the display symbology are discussed and analyzed to identify potential areas of improvement.
机译：已经开发了一种用于推进和机身控制的综合方法，并使用NASA Lewis研究中心的固定基础飞行模拟器对短距起飞垂直着陆（STOVL）飞机进行了评估。为了进行此评估，将飞行模拟器配置为使用STOVL飞机模型，全非线性涡扇发动机模型，模拟座舱和显示器以及飞行员效应器进行过渡飞行。本文简要介绍了仿真模型，飞行仿真环境，显示和符号系统，集成控制设计以及用于控制设计评估的飞行员任务。在模拟中，飞行员成功地完成了典型的过渡阶段任务，例如恒定减速与飞行路径跟踪相结合，以及恒定加速度起降机动。讨论并分析了有关集成系统性能和显示符号的试验性意见，以确定潜在的改进领域。

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