Fuel-Saving Climb Procedure by Reduced Thrust near Top of Climb-Reference-Cited by-同舟云学术

Fuel-Saving Climb Procedure by Reduced Thrust near Top of Climb

Published:2020-09 Issue:5 Volume:57 Page:800-806
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Mori R.¹

Affiliation:

1. Electronic Navigation Research Institute, Tokyo 182-0012, Japan

Funder

JSPS KAKENHI

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference15 articles.

1. Benefit Potential of Continuous Climb and Descent Operations

2. Optimal Airspace Design for Continuous Climb Operation

3. A Terminal Area Analysis of Continuous Ascent Departure Fuel Use at Dallas/Fort Worth International Airport

4. Aircraft performance optimization.

5. ErzbergerH. “Optimum Climb and Descent Trajectories for Airline Missions,” AGARD Theory and Application of Optimal Control in Aerospace Systems, AGARDograph No. 251, 1981.

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