DocumentCode
592923
Title
Study on Evaluation Technology of Airborne Electrical System Based on Physical Test
Author
Liang Xu ; Wen Feifei ; Guo Hong ; Dong Bigui
Author_Institution
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fYear
2012
fDate
8-10 Dec. 2012
Firstpage
211
Lastpage
214
Abstract
Airborne electrical system is a key part of the airborne systems of advanced helicopter, and becomes more and more complicated. In order to evaluate the comprehensive design performance of airborne electrical system effectively, this paper discusses the corresponding principle and method to establish the perfect objective evaluation architecture based on the physical test.
Keywords
aircraft power systems; aircraft testing; helicopters; advanced helicopter; airborne electrical system; evaluation technology; perfect objective evaluation architecture; physical test; Atmospheric modeling; Computer architecture; Indexes; Mathematical model; Power supplies; Steady-state; Transient analysis; Airborne electrical system; Evaluation; National Military standard; Physical test;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2012 Second International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4673-5034-1
Type
conf
DOI
10.1109/IMCCC.2012.56
Filename
6428888
Link To Document