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Development of Possible Go-Around Criteria for Transport Aircraft

机译:制定运输飞机可能的复飞标准

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This paper adds data to help with the development of possible go-around criteria for transport category aircraft. Presently, airline procedures state that pilots make a go-around decision using multiple criteria at 1000 or 500 ft above the ground, or so-called gates. An experiment conducted on three level-D full-flight simulators investigated the conditions from which pilots cannot successfully recover from an unstable approach and make a normal landing. In addition, pilots' perceptions of risk under these various unstable approach conditions and resulting landings were assessed. Six crews, comprised of a captain and a first officer from the same airline, participated in each simulator. Both the captain and the first officer flew approaches and landings from 55 different initial conditions with varying gate heights, localizer deviations, glideslope deviations, reference-speed deviations, and rate of descents. The initial condition at the starting gate mainly affected longitudinal touchdown deviation and rate of descent at touchdown, with reference-speed deviation having the most significant effect Results show little difference in touchdown performance for conditions from the 300-ft and 500-ft gates. Conditions at the 100-ft gate introduced significant differences in touchdown performance. Reference-speed and localizer deviation at the starting gate had the strongest influences on perceived risk and go-around decision. In line with other studies, these findings suggest that a 300-ft go-around gate might be acceptable. More research is required to investigate the effects of environmental and runway variables before possible go-around criteria for transport category aircraft can be defined.
机译:本文添加了数据,以帮助制定运输类飞机可能的复飞标准。目前,航空公司程序规定,飞行员使用地面以上1000或500英尺的多个标准或所谓的登机口做出复飞决定。在三个D级全飞行模拟器上进行的实验研究了飞行员无法从不稳定进场中成功恢复并正常降落的条件。此外,还评估了飞行员在各种不稳定进近条件下以及由此导致的着陆情况下的风险感知。六名机组人员由同一航空公司的机长和副驾驶组成,他们参加了每个模拟器。机长和副驾驶都从55种不同的初始条件飞入和着陆,并且门高度,定位器偏差,滑坡偏差,参考速度偏差和下降率均发生变化。起始闸门的初始条件主要影响纵向着陆偏差和着陆时的下降速率,而参考速度偏差的影响最大。结果表明,对于300英尺和500英尺闸门而言,着陆性能几乎没有差异。 100英尺登机口的条件在接地性能方面带来了显着差异。起跑门处的参考速度和定位器偏差对感知的风险和复飞决策影响最大。与其他研究一致,这些发现表明300英尺的复飞门可能是可以接受的。在可以定义运输类飞机可能的复飞标准之前,需要进行更多的研究以调查环境和跑道变量的影响。

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