{"title":"Helicopter and avionics systems electromagnetic environmental effects","authors":"D. Millard, T. A. Torres","doi":"10.1109/DASC.1990.111260","DOIUrl":null,"url":null,"abstract":"It is shown that adverse electromagnetic environmental effects (E/sup 3/) can be reduced during the configuration of military helicopters by implementing a complete helicopter E/sup 3/ program. The E/sup 3/ 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 E/sup 3/ engineering effort through an electromagnetic compatibility advisory board. The avionics configuration analysis program, a computer-aided engineering tool to accomplish the E/sup 3/ analysis, and the ribbonized organized integrated wiring concept are presented.<<ETX>>","PeriodicalId":141205,"journal":{"name":"9th IEEE/AIAA/NASA Conference on Digital Avionics Systems","volume":"13 2","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1990-10-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"9th IEEE/AIAA/NASA Conference on Digital Avionics Systems","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/DASC.1990.111260","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
It is shown that adverse electromagnetic environmental effects (E/sup 3/) can be reduced during the configuration of military helicopters by implementing a complete helicopter E/sup 3/ program. The E/sup 3/ 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 E/sup 3/ engineering effort through an electromagnetic compatibility advisory board. The avionics configuration analysis program, a computer-aided engineering tool to accomplish the E/sup 3/ analysis, and the ribbonized organized integrated wiring concept are presented.<>