EXPERIMENTAL APPROACH FOR EFFICIENT ARRIVAL PROCEDURES WITH FIXED-FLIGHT PATH ANGLE DESCENT

被引:0
|
作者
Wickramasinghe, Navinda K. [1 ]
Toratani, Daichi [1 ]
Itoh, Eri [1 ]
Westphal, Jendrick [2 ]
Schoniger, Hendrik [2 ]
Feuerle, Thomas [3 ]
Stanisak, Mirko [3 ]
机构
[1] Elect Nav Res Inst, Natl Inst Maritime Port & Aviat Technol, Tokyo, Japan
[2] Jeppesen GmbH, Neu Isenburg, Germany
[3] Tech Univ Carolo Wilhelmina Braunschweig, Braunschweig, Germany
关键词
D O I
10.1109/icnsurv.2019.8735118
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Increasing the throughput at major airports with efficient air traffic flow management is a daunting challenge and efficient arrival procedures with increased predictability are key to address these demands. In a preceding study, authors proposed a conceptual framework on an integrated system of Fixed-flight Path Angle (FPA) and GBAS Landing System (GLS) as an augmentation to Continuous Descent Operation (CDO), which is considered to be a potential mitigation strategy for both fuel consumption and environmental impact. This paper provides an experimental approach to review key aspects for implementing FPA descent procedures in real operational environment and to explore the possibility of integrating such a procedure with next-generation approach systems. Design methodology for FPA descent is explained by referring to FPA descent trajectories simulated from a trajectory generator developed by the authors. Results from a series of full-flight simulator trials are investigated for the procedure's feasibility, pilot workload and potential benefits compared to conventional descent procedures. A case study conducted as a part of the Jeppesen's digital airline / 59+1 technical demonstration under the Boeing's ecoDemonstrator 2018 Program is also reviewed. Results show that the ground-based trajectory prediction could be achieved with significant accuracy by integrating two deceleration segments to the FPA procedure design.
引用
收藏
页数:14
相关论文
共 22 条
  • [1] Experimental Approach for Efficient Arrival Procedures with Fixed-Flight Path Angle Descent
    Wickramasinghe, N. K.
    Toratani, D.
    Itoh, E.
    Westphal, J.
    Schoniger, H.
    Feuerle, T.
    Stanisak, M.
    [J]. 2019 INTEGRATED COMMUNICATIONS, NAVIGATION AND SURVEILLANCE CONFERENCE (ICNS), 2019,
  • [2] Feasibility Study on Efficient Arrival Operations via the Integration of Fixed-Flight Path Angle Descent and GBAS Landing System
    Wickramasinghe, Navinda K.
    Itoh, Eri
    Toratani, Daichi
    Westphal, Jendrick
    Schoniger, Hendrik
    Feuerle, Thomas
    Stanisak, Mirko
    Schachtebeck, Per M.
    Fukushima, Sonosuke
    Saito, Susumu
    Yoshihara, Takayuki
    [J]. 2017 IEEE/AIAA 36TH DIGITAL AVIONICS SYSTEMS CONFERENCE (DASC), 2017,
  • [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
  • [4] Feasibility study on fixed flight-path angle descent for wide-body passenger aircraft
    Itoh E.
    Wickramasinghe N.K.
    Hirabayashi H.
    Fukushima S.
    [J]. CEAS Aeronautical Journal, 2019, 10 (02) : 589 - 612
  • [5] 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
  • [6] Descent profille options for continuous descent arrival procedures within 3D path concept
    Tong, Kwok-On
    Schoemig, Ewald G.
    Boyle, Danial A.
    Scharl, Julien
    Haraldsdottir, Aslaug
    [J]. 2007 IEEE/AIAA 26TH DIGITAL AVIONICS SYSTEMS CONFERENCE, VOLS 1-3, 2007, : 437 - 447
  • [7] NOx, fuel consumption and time effects of flight path angle during descent
    Turgut, Enis T.
    Usanmaz, Oznur
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2013, 227 (G5) : 737 - 750
  • [8] 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
  • [9] A Preliminary Study on Relationship between Flight Path Angle and NOx Emissions during Descent
    Turgut, Enis T.
    Usanmaz, Oznur
    Kahvecioglu, Sinem
    Rosen, Marc A.
    [J]. SDEWES: THE 8TH CONFERENCE ON SUSTAINABLE DEVELOPMENT OF ENERGY, WATER AND ENVIRONMENT SYSTEMS, 2014, 42 : 109 - 114
  • [10] Empirical analysis of the effect of descent flight path angle on primary gaseous emissions of commercial aircraft
    Turgut, Enis T.
    Usanmaz, Oznur
    Rosen, Marc A.
    [J]. ENVIRONMENTAL POLLUTION, 2018, 236 : 226 - 235