DocumentCode
2260068
Title
Aircraft turbine engine control systems development: Historical perspective
Author
Lutambo, Jackson ; Wang, Jiqiang ; Yue, Hong ; Dimirovsky, Georgi
Author_Institution
Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China
fYear
2015
fDate
28-30 July 2015
Firstpage
5736
Lastpage
5741
Abstract
This paper describes the development of aircraft turbine engine control systems from the historical point of view to the present. With the increasing emphasis on aircraft safety, enhanced performance, and affordability, as well as the need to reduce the environmental effect caused by aircraft, there are many new challenges being faced by the designers of aircraft propulsion systems. The paper provides an overview of the various technological development activities in aircraft engine control and diagnostics, both current and some accomplished in the recent past. The motivations for each of the research efforts, the research approach, technical challenges, and the key progress to date are summarized.
Keywords
DVD; Decision support systems; Control system; Digital Electronic Engine Control (DEEC); FullAuthority Digital Electronic Control (FADEC); Gas Turbine Engine; Hydromechanical System;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2015 34th Chinese
Conference_Location
Hangzhou, China
Type
conf
DOI
10.1109/ChiCC.2015.7260534
Filename
7260534
Link To Document