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Feasibility study on fixed flight-path angle descent for wide-body passenger aircraft

机译:宽体乘用车固定飞行路径角度下降的可行性研究

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摘要

This study proposes the use of fixed flight-path angle (FPA) descent as a potential alternative for eco-friendly air traffic operations. Additionally, given that the proposed descent procedure follows a fixed, assigned flight-path angle, with the aircraft continuously descending toward the runway threshold with near-idle thrust, the trajectory should be more predictable for air-traffic controllers. As such, the proposed approach is expected to contribute significantly toward decreasing the air traffic fuel consumption, while simultaneously facilitating the air traffic controllers' task of maintaining the required time spacing between concurrent traffic. Furthermore, FPA descent does not require any retrofits in the fundamental components of current ground systems and/or onboard avionics. This paper clarifies the feasibility of fixed flight-path angle descent for B777-200 and B787-8 wide-body jet passenger aircraft, envisaging its implementation in near-term operations. A total of 30 trials were carried out in a series of experiments designed to evaluate the proposed descent method, considering arrivals at two major international airports in Japan-the Tokyo and Kansai International Airports-using B777-200 and B787-800 full flight simulators of a national airline. The pilots' procedures, cockpit operability, assigned vertical path tracking performance, and fuel efficiency associated with the proposed FPA descent are discussed and compared with those of conventional arrival operations. The analysis results indicate that the fixed flight-path angle descent is feasible for large-sized jet aircraft within the assumed operational environment, and that its combined use with speed control has the potential to result in even better energy-saving performance in future air traffic management operations.
机译:本研究提出使用固定的飞行路径角(FPA)下降作为环保空中交通运营的潜在替代方案。另外,考虑到所提出的下降程序遵循固定的,分配的飞行路径角,并且飞机连续下降朝向近怠速推力的跑道阈值,轨迹应该更加可预测空气交通控制器。因此,预计所提出的方法将大大促进减少空中交通燃料消耗,同时促进空中交通管制员的任务,以维护并发流量之间所需的时间间距。此外,FPA血液不需要在当前地面系统和/或船上航空电子设备的基本组件中进行任何改造。本文阐明了B777-200和B787-8宽体喷射客机的固定飞行路径角度下降的可行性,设想其在近期运营中的实施。在一系列实验中进行了共有30项试验,旨在评估拟议的血统方法,考虑到日本两大国际机场的到达 - 东京和关西国际机场 - 使用B777-200和B787-800全飞行模拟器国家航空公司。讨论了导频程序,驾驶舱可操作性,分配的垂直路径跟踪性能和与所提出的FPA下降相关的燃料效率与传统到达操作的常规运营进行比较。分析结果表明,固定的飞行路径角度下降对于假定的操作环境中的大型喷射机是可行的,并且其与速度控制的结合使用具有可能导致未来的空中交通中的更好的节能性能。管理运营。

著录项

  • 来源
    《CEAS Aeronautical Journal》 |2019年第2期|589-612|共24页
  • 作者单位

    Air Traffic Management Department Electronic Navigation Research Institute National Institute of Maritime Port and Aviation Technology 7-42-23 Jindaiji-Higashimachi Chofu Tokyo 182-0012 Japan;

    Air Traffic Management Department Electronic Navigation Research Institute National Institute of Maritime Port and Aviation Technology 7-42-23 Jindaiji-Higashimachi Chofu Tokyo 182-0012 Japan;

    Air Traffic Management Department Electronic Navigation Research Institute National Institute of Maritime Port and Aviation Technology 7-42-23 Jindaiji-Higashimachi Chofu Tokyo 182-0012 Japan;

    Air Traffic Management Department Electronic Navigation Research Institute National Institute of Maritime Port and Aviation Technology 7-42-23 Jindaiji-Higashimachi Chofu Tokyo 182-0012 Japan;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Air traffic management; Continuous descent operation; Flight simulator experiments; Fuel reduction; Asian economic growth;

    机译:空中交通管理;连续下降操作;飞行模拟器实验;减少燃油;亚洲经济增长;
  • 入库时间 2022-08-18 21:48:32

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