DocumentCode :
146388
Title :
Modeling of propeller electric airplane and thrust control using advantage of electric motor
Author :
Takahashi, Koichi ; Fujimoto, Hiroshi ; Hori, Yoichi ; Kobayashi, Hideo ; Nishizawa, A.
Author_Institution :
Grad. Sch. of Frontier Sci., Univ. of Tokyo, Kashiwa, Japan
fYear :
2014
fDate :
14-16 March 2014
Firstpage :
482
Lastpage :
487
Abstract :
Electrical airplanes (EAs) have become practical in the recent years. Considering the increase of demand on smaller aircraft and the attention to environmental issues, the demand on small EAs is expected to grow in the coming decade. However, the accident rate of small aircrafts is higher than that of larger aircrafts, so ensuring higher safety of EA is very urgent. In this paper, the new thrust control method based on new EA propeller plant is proposed. This method can be applied to new advanced flight control systems of EA, which can be expected to improve the safety of EA. The effectiveness of the proposed method is verified through simulations and experiments.
Keywords :
aerospace accidents; aircraft control; electric motors; propellers; EA propeller plant; accident rate; aircraft; electric motor; flight control system; propeller electric airplane; thrust control method; Airplanes; Atmospheric modeling; Mathematical model; Propellers; Radiation detectors; Torque; Vectors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Advanced Motion Control (AMC),2014 IEEE 13th International Workshop on
Conference_Location :
Yokohama
Type :
conf
DOI :
10.1109/AMC.2014.6823329
Filename :
6823329
Link To Document :
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