Feasibility analyses for paired approach procedures for closely spaced parallel runways

R. Eftekari, J. Hammer, D. Havens, A. Mundra
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引用次数: 13

Abstract

In current air traffic operations in the U.S., closely spaced parallel runways (CSPRs) separated by less than 2500 feet (ft) can be used to conduct simultaneous parallel operations using visual separation. Once below visual approach minima, such dual runway operations are no longer possible. To address this loss of throughput, several concepts are currently under consideration. This paper discusses a “paired approach” concept which enables use of CSPRs down to Category I and II approach minima. The paper documents Monte Carlo analyses on the feasibility and trade-offs of paired approach procedure variants with and without an escape maneuver. It concludes that both procedure variations require echelon staggering for most airports with runway centerline (RCL) separations below 2500 ft and provides window parameters required for an acceptable Target Level of Safety (TLS). It shows that a value of up to 4000 ft for this echelon spacing is adequate for most CSPRs for an adverse wind threshold of 10 knots; the specific value depending on the concept variation and geometry. Other findings include the ability to achieve abeam positioning with an escape procedure for several runway configurations. Many procedural combinations examined are capable of pairing 95% to 100% of aircraft. Additionally, this paper presents an analysis of wake encounter risk during blunders. The analysis results suggest the non-escape procedure variant has a high probability of wake vortex encounter during blunder. On the other hand, the escape procedure variant with a delay in breakout of 8 seconds or less appears to provide protection from wake encounters even during a blunder. Preliminary considerations for surveillance requirements are presented, including optional 1090 MHz Extended Squitter (1090ES) Automatic Dependent Surveillance-Broadcast (ADS-B) messages and fields that may support the escape procedure variation.
紧密间隔平行跑道成对进近程序的可行性分析
在美国目前的空中交通操作中,间距小于2500英尺(ft)的紧密平行跑道(CSPRs)可以使用视觉分离来进行同时平行操作。一旦低于目视进近最低限度,这种双跑道操作就不再可能。为了解决这种吞吐量损失,目前正在考虑几个概念。本文讨论了一种“配对方法”概念,该概念使CSPRs的使用达到了第一类和第二类方法的最小值。本文用蒙特卡罗方法分析了带和不带逃逸机动的配对接近程序变量的可行性和权衡。结论是,对于大多数跑道中心线(RCL)距离低于2500英尺的机场,这两种程序变化都需要梯队交错,并提供了可接受的目标安全级别(TLS)所需的窗口参数。结果表明,在10节的逆风阈值下,对于大多数CSPRs来说,高达4000英尺的梯队间距是足够的;具体数值取决于概念变化和几何形状。其他发现还包括在几种跑道配置中使用逃生程序实现纵梁定位的能力。经过检验的许多程序组合能够配对95%到100%的飞机。此外,本文还对失误时尾流遭遇风险进行了分析。分析结果表明,非逃逸程序变体在碰撞过程中遇到尾流涡的概率很高。另一方面,在8秒或更少的爆发延迟的逃脱程序变体似乎提供保护,从尾流遭遇,即使在一个错误。提出了对监视要求的初步考虑,包括可选的1090 MHz扩展分频器(1090ES)自动相关监视广播(ADS-B)消息和可能支持逃逸程序变化的字段。
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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