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A piloted simulation investigation of several command concepts for transport aircraft in the approach and landing

机译:在进近和着陆时对运输机的几种指挥概念进行的模拟试验研究

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摘要

With the introduction of modern fly-by-wire aircraft, the response of an aircraft to a pilot’s input can be augmented to something other than that for a conventional aircraft, with the resultant benefits and problems. The issue of what commanded response a pilot desires has received considerable attention, however no clear conclusions have yet emerged.The requirements for up and away flight and for the flare and landing seem to be different. Away from the ground rate command systems such as pitch rate and flight path rate seem to be well received for their low pilot workload associated with the control of flight path. However in the flare and touchdown these systems exhibit unnatural floating tendencies, requiring the pilot to push forward on the stick to land the aircraft. As a result most fly-by-wire aircraft incorporate separate up and away control laws and flare laws.This investigation is designed to consolidate on the work achieved by many organisations over the past ten years and concentrate on pilots’ preferences for the final stages of the approach and into the flare and touchdown.Twenty nine different flight control law configurations were designed for a regional sized aircraft. These configurations concentrated on several different command philosophies designed to investigate the pilots’ preferred command parameter and covered three different centre of gravity locations. These configurations were then implemented on the fixed base engineering simulator at British Aerospace Regional Aircraft, Hatfield, and evaluated by four test pilots.
机译:随着现代电传操纵飞机的引入,飞机对飞行员输入的反应可以增强到常规飞机以外的其他方式,从而带来好处和问题。飞行员希望获得什么样的命令响应的问题已经引起了相当多的关注,但是尚未得出明确的结论。对上下飞行以及耀斑和着陆的要求似乎有所不同。诸如俯仰率和飞行路径速率之类的地面速率指令系统似乎因其与飞行路径控制相关的飞行员工作量低而受到广泛好评。但是,在耀斑和着陆时,这些系统表现出不自然的漂浮趋势,需要飞行员向前推动以使飞机降落。结果,大多数电传飞行飞机都采用了单独的上,下控制法和耀斑法。本调查旨在巩固许多组织在过去十年中所做的工作,并着重于飞行员对飞机最后阶段的偏好针对一架区域性飞机设计了29种不同的飞行控制法则配置。这些配置集中在几种不同的指挥理念上,旨在研究飞行员的首选指挥参数,并涵盖了三个不同的重心位置。然后,在哈特菲尔德的英国航空区域飞机公司的固定基础工程仿真器上实施了这些配置,并由四名测试飞行员进行了评估。

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    Field Edmund;

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  • 年度 1994
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  • 原文格式 PDF
  • 正文语种 en_UK
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