DocumentCode :
2592217
Title :
Helicopter and avionics systems electromagnetic environmental effects
Author :
Millard, David P. ; Torres, Thomas A.
Author_Institution :
Georgia Inst. of Technol., Atlanta, GA, USA
fYear :
1990
fDate :
15-18 Oct 1990
Firstpage :
47
Lastpage :
52
Abstract :
It is shown that adverse electromagnetic environmental effects (E 3) can be reduced during the configuration of military helicopters by implementing a complete helicopter E3 program. The E3 program methodology includes: defining the electromagnetic environment (EME) in which the helicopter must operate and survive during all phases of its mission; analyzing the performance of the helicopters avionics systems in the EME and correcting deficiencies in both Group A (interface) and Group B (boxes) systems; testing the electromagnetic vulnerability of the helicopter in the EME: and documenting the entire E3 engineering effort through an electromagnetic compatibility advisory board. The avionics configuration analysis program, a computer-aided engineering tool to accomplish the E 3 analysis, and the ribbonized organized integrated wiring concept are presented
Keywords :
aerospace computing; aerospace testing; aircraft instrumentation; electromagnetic compatibility; electromagnetic interference; helicopters; military systems; EMC; EMI; Group A; Group B; avionics; computer-aided engineering; degradation; electrical interconnect system; electromagnetic compatibility; electromagnetic environment; electromagnetic environmental effects; electromagnetic vulnerability; interface; military helicopters; ribbonized organized integrated wiring; testing; Aerospace electronics; Computer aided engineering; Databases; Electromagnetic analysis; Electromagnetic compatibility; Helicopters; Military aircraft; Performance analysis; Performance evaluation; Wiring;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
Conference_Location :
Virginia Beach, VA
Type :
conf
DOI :
10.1109/DASC.1990.111260
Filename :
111260
Link To Document :
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