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Piloted Simulation Evaluation of Tracking MTEs for the Assessment of High-Speed Handling Qualities

机译:跟踪MTE的先导仿真评估,以评估高速处理质量

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Updates to the military rotorcraft handling qualities specification are currently being considered that address the high-speed flight regime envisioned for the Future Vertical Lift platform of the US Army. A team that features industry and academia have developed and evaluated a set of Mission Task Elements (MTEs) that are defined to address VTOL high-speed handling qualities. Following the mission-oriented approach upon which ADS-33E-PRF is based, the MTEs were designed to meet different levels of precision and aggressiveness. Tracking MTEs based on a sum-of-sinewaves (SOS) command signal were defined for precision, aggressive and precision, non-aggressive applications. The command signals are derived from fixed wing analogs that have long been used to evaluate aircraft handling qualities. While the precision, aggressive SOS tracking tasks, the primary subject of this paper, are surrogates for air-to-air tracking and nap-of-the-earth tracking, the known forcing function allows for complete open- and closed-loop pilot-vehicle system identification. The MTE objectives, descriptions, and performance criteria were assessed and refined via several checkout piloted simulation sessions. Formal evaluations were then conducted by Army test pilots at four simulator facilities, each featuring a unique high-speed platform including a generic winged compound helicopter, two tiltrotor configurations, and a compound helicopter with coaxial rotors. To aid in the MTE evaluation process, baseline VTOL configurations were varied to achieve different handling qualities levels. Quantitative measures based on task performance and qualitative measures based on pilot ratings, comments and debrief questionnaires were used to assess MTE effectiveness. The piloted simulation results demonstrated that the sum-of-sines tracking MTEs provided an effective means to discern precision, aggressive handling qualities in high speed flight.
机译:目前正在考虑对军用旋翼飞机的操纵质量规范进行更新,以解决为美国陆军未来垂直升降平台所设想的高速飞行体制。一个由行业和学术界组成的团队开发并评估了一组任务任务元素(MTE),这些任务元素旨在解决VTOL的高速处理质量。遵循以ADS-33E-PRF为基础的面向任务的方法,MTE的设计满足了不同水平的精度和攻击性要求。定义了基于正弦波和(SOS)命令信号的跟踪MTE,用于精确,主动和精确,非攻击性应用。指令信号来自长期以来用于评估飞机操纵质量的固定机翼类似物。虽然精确,激进的SOS跟踪任务(本文的主要主题)是空对空跟踪和小睡跟踪的替代方法,但已知的强制功能可实现完整的开环和闭环飞行员控制。车辆系统识别。 MTE的目标,描述和性能标准是通过几次结帐试点模拟会议进行评估和完善的。然后,陆军测试飞行员在四个模拟器设施上进行了正式评估,每个设施都具有一个独特的高速平台,其中包括一架通用翼复合直升机,两个俯仰旋翼配置以及一架带同轴旋翼的复合直升机。为了协助MTE评估过程,对基线VTOL配置进行了更改,以实现不同的处理质量级别。基于任务绩效的定量方法和基于飞行员等级,评论和汇报调查表的定性方法用于评估MTE的有效性。试点模拟结果表明,正弦和跟踪MTE提供了一种有效的手段,可以识别高速飞行中的精确,激进的操纵质量。

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