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