{"title":"直升机和航空电子系统电磁环境影响","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":"{\"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}","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}
Helicopter and avionics systems electromagnetic environmental effects
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.<>