Reduced Thrust Take-off Control Law Design for Large Commercial Aircraft

DOI

10.2991/icmmbe-16.2016.76How to use a DOI?

Keywords

Reduced Thrust Takeoff, Assumed Temperature, Derate Method

Abstract

As the actual take-off weight of the aircraft is less than the maximum take-off weight, the technology utilizing thrust less than maximum take-off thrust for take-off is called reduced thrust take-off. Reduced thrust take-off is in generally divided into Assumed Temperature and Derate Method. In this paper, the principle of reduced thrust take-off is analyzed, and the method combined Assumed Temperature and Derate Method is studied. At last, the vertical control law of reduced thrust take-off which combines. Assumed Temperature and Derate Method is designed and simulated for a large commercial aircraft. The results show, under the correct flight circumstances, reduced thrust take-off researched is very important to improve the economic benefits of the airline, which can reduce operating costs of the airline, improve engine life and reduce fuel consumption.

Copyright

© 2016, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Haitao Yin
AU  - Yan Li
PY  - 2016/09
DA  - 2016/09
TI  - Reduced Thrust Take-off Control Law Design for Large Commercial Aircraft
BT  - Proceedings of the6th International Conference on Mechatronics, Materials, Biotechnology and Environment (ICMMBE 2016)
PB  - Atlantis Press
SP  - 404
EP  - 409
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmmbe-16.2016.76
DO  - 10.2991/icmmbe-16.2016.76
ID  - Yin2016/09
ER  -