Reduced Thrust Take-off Control Law Design for Large Commercial Aircraft
- 10.2991/icmmbe-16.2016.76How to use a DOI?
- Reduced Thrust Takeoff, Assumed Temperature, Derate Method
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.
- © 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/).
Cite this article
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 -