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 :
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