experimental aircraft, MuPAL, multi purpose aviation laboratory, engine response, engine torque, power lever input, mathematical model, fly by wire system, flight test, in flight simulator
その他のタイトル（英）
Flight tests for engine torque response of Dornier Do-228
National Aerospace Laboratory Flight Research Division
National Aerospace Laboratory Flight Research Division
National Aerospace Laboratory Flight Research Division
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory (NAL)
雑誌名
航空宇宙技術研究所資料
雑誌名(英)
Technical Memorandum of National Aerospace Laboratory
A Dornier Do-228, one of the experimental aircrafts of NAL, is to be modified into an in-flight simulator, named MuPAL (Multi-Purpose Aviation Laboratory). In order to develop the thrust control law for its Fly-By-Wire system, the engine response of the original Do-228 for power lever input is needed to know. This report describes the results of flight tests on the Do-228's engine torque response and constructs its mathematical model from the flight test data.
ドルニエDo-228型機のエンジン出力トルク応答特性の飛行実験
naltm0000723.pdf
(627.94KB)
