Description and flight test of a rollout and turnoff (ROTO) head-up display (HUD) guidance system

R.M. Hueschen, W. W. Hankins, L. K. Barker
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引用次数: 8

Abstract

The ROTO system provided guidance that resulted in mean ROT values essentially the same as those for current clear-weather operations and standard deviation ROT values a factor of 1.5 to 2.0 less (depending on exit comparison). Assuming the pilots can follow the guidance in low visibility conditions, these ROT values imply that clear-weather runway capacity could be maintained in low visibility conditions. All the pilots liked the system and found the guidance easy to follow after a couple of training runs. In general, the pilots were able to control the aircraft ground speed along the runway to within 10 knots of commanded ground speed from the ROTO guidance.
一种滚转(ROTO)平视显示(HUD)制导系统的描述和飞行试验
ROTO系统提供的指导结果显示,平均ROT值与当前晴空作业的ROT值基本相同,而标准偏差ROT值则少1.5至2.0倍(取决于出口比较)。假设飞行员可以在低能见度条件下跟随引导,这些ROT值意味着在低能见度条件下可以保持晴空跑道容量。所有的飞行员都喜欢这个系统,经过几次训练后,他们发现指导很容易遵循。一般来说,飞行员能够控制飞机沿跑道的地面速度到从ROTO制导的命令地面速度的10节以内。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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