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

被引:1
|
作者
Itoh E. [1 ]
Wickramasinghe N.K. [1 ]
Hirabayashi H. [1 ]
Fukushima S. [1 ]
机构
[1] Air Traffic Management Department, Electronic Navigation Research Institute, National Institute of Maritime, Port and Aviation Technology, 7-42-23 Jindaiji-Higashimachi, Chofu, 182-0012, Tokyo
关键词
Air traffic management; Asian economic growth; Continuous descent operation; Flight simulator experiments; Fuel reduction;
D O I
10.1007/s13272-018-0337-9
中图分类号
学科分类号
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. © 2018, The Author(s).
引用
收藏
页码:589 / 612
页数:23
相关论文
共 27 条
  • [1] Effects of Descent Flight-Path Angle on Fuel Consumption of Commercial Aircraft
    Turgut, Enis T.
    Usanmaz, Oznur
    Cavcar, Mustafa
    Dogeroglu, Tuncay
    Armutlu, Kadir
    [J]. JOURNAL OF AIRCRAFT, 2019, 56 (01): : 313 - 323
  • [2] Feasibility study on applying continuous descent operations in congested airspace with speed control functionality: Fixed flight-path angle descent
    Toratani, Daichi
    Wickramasinghe, Navinda Kithmal
    Westphal, Jendrick
    Feuerle, Thomas
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 107
  • [3] Demonstration of Fixed Flight-Path Angle Descent via Scheduled Commercial Flights
    Iwata, Daiki
    Nonaka, Yuki
    Funai, Yasunobu
    Shindo, Takehiko
    Tanaka, Shinji
    Sato, Makoto
    Itoh, Eri
    [J]. Journal of Air Transportation, 2024, 32 (03): : 130 - 145
  • [5] Monitoring microbial populations on wide-body commercial passenger aircraft
    Mckernan, Lauralynn Taylor
    Wallingford, Kenneth M.
    Hein, Misty J.
    Burge, Harriet
    Rogers, Christine A.
    Herrick, Robert
    [J]. ANNALS OF OCCUPATIONAL HYGIENE, 2008, 52 (02): : 139 - 149
  • [6] Distributed Control for Flight-path Angle Synchronized Tracking of Multiple Fixed-wing Aircraft
    Zhu, Yang
    Zhu, Bo
    Qin, Kai-Yu
    Liu, Hugh Hong-Tao
    [J]. 2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2016, : 312 - 317
  • [7] Evaluating energy-saving arrivals of wide-body passenger aircraft via flight-simulator experiments
    [J]. Itoh, Eri, 1600, AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States (55):
  • [8] Evaluating Energy-Saving Arrivals of Wide-Body Passenger Aircraft via Flight-Simulator Experiments
    Itoh, Eri
    Fukushima, Sachiko
    Hirabayashi, Hiroko
    Wickramasinghe, Navinda K.
    Toratani, Daichi
    [J]. JOURNAL OF AIRCRAFT, 2018, 55 (06): : 2427 - 2443
  • [9] Flight Dynamic Characteristics of Wide-Body Aircraft with Wind Gust and Turbulence
    Mehmood, Kashif
    Ali Shah, Syed Irtiza
    Ali Shams, Taimur
    Mumtaz Qadri, Muhammad Nafees
    Khan, Tariq Amin
    Kukulka, David
    [J]. FLUIDS, 2023, 8 (12)
  • [10] The Study Of Wide-body Aircraft Family Using NSGAII
    Ding, Songbin
    Ge, Ruichen
    Gu, Qianqian
    Wang, Xiaoli
    [J]. 2016 8TH INTERNATIONAL CONFERENCE ON ELECTRONICS, COMPUTERS AND ARTIFICIAL INTELLIGENCE (ECAI), 2016,