DocumentCode
2840552
Title
Aircraft test conditions for electromagnetic compatibility assessment
Author
Redman, M.B.
fYear
1996
fDate
35380
Firstpage
42401
Lastpage
42408
Abstract
Before electromagnetic compatibility (EMC) testing of whole aircraft can be carried out, all of the requirements must be clearly defined. In particular, the objectives must be set out and the flight critical systems determined to allow the EMC assessment to be performed in as near representative condition of flight as possible. This will give the confidence when the withstand capability of the aircraft is measured, during exposure to its own on-board radio frequency (RF) environment and to the external RF environment in which it is to operate. This paper discusses those aspects of relating to the aircraft test conditions prior to the EMC assessment. In addition, the use of the accident data recorder (ADR) is discussed as a useful tool in the EMC assessment programme, which can, if required, be used for flight test assessment as well as ground trials, without the need of additional specialist instrumentation
fLanguage
English
Publisher
iet
Conference_Titel
EMC (Electromagnetic Compatibility) in Aerospace (Digest No.: 1996/243), IEE Colloquium on
Conference_Location
London
Type
conf
DOI
10.1049/ic:19961298
Filename
640321
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