{"title":"研究了有意超短电磁脉冲对飞机电子系统干扰的抗扰性","authors":"R. Gaynutdinov, S. Chermoshentsev","doi":"10.1109/APEDE.2016.7878983","DOIUrl":null,"url":null,"abstract":"An approach based on the electromagnetic topology method for predicting immunity to disturbance of electronic system aircraft at the influence of intentional ultrashort electromagnetic impulses is discussed. Aircraft for small aircraft a fuselage and tail, which are made of composite material, are considered. An example prediction of immunity to disturbance of electronic aircraft control system and recommendations to ensure immunity to disturbance at the influence of intentional ultrashort electromagnetic pulses is discusses.","PeriodicalId":231207,"journal":{"name":"2016 International Conference on Actual Problems of Electron Devices Engineering (APEDE)","volume":"23 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"8","resultStr":"{\"title\":\"Study immunity to disturbance of electronic system aircraft by influences of intentional ultrashort electromagnetic pulses\",\"authors\":\"R. Gaynutdinov, S. Chermoshentsev\",\"doi\":\"10.1109/APEDE.2016.7878983\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"An approach based on the electromagnetic topology method for predicting immunity to disturbance of electronic system aircraft at the influence of intentional ultrashort electromagnetic impulses is discussed. Aircraft for small aircraft a fuselage and tail, which are made of composite material, are considered. An example prediction of immunity to disturbance of electronic aircraft control system and recommendations to ensure immunity to disturbance at the influence of intentional ultrashort electromagnetic pulses is discusses.\",\"PeriodicalId\":231207,\"journal\":{\"name\":\"2016 International Conference on Actual Problems of Electron Devices Engineering (APEDE)\",\"volume\":\"23 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"8\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 International Conference on Actual Problems of Electron Devices Engineering (APEDE)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/APEDE.2016.7878983\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 International Conference on Actual Problems of Electron Devices Engineering (APEDE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/APEDE.2016.7878983","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Study immunity to disturbance of electronic system aircraft by influences of intentional ultrashort electromagnetic pulses
An approach based on the electromagnetic topology method for predicting immunity to disturbance of electronic system aircraft at the influence of intentional ultrashort electromagnetic impulses is discussed. Aircraft for small aircraft a fuselage and tail, which are made of composite material, are considered. An example prediction of immunity to disturbance of electronic aircraft control system and recommendations to ensure immunity to disturbance at the influence of intentional ultrashort electromagnetic pulses is discusses.