{"title":"航天飞机导航系统的工作原理及消光脉冲损耗","authors":"C. Tsang","doi":"10.1109/AERO.1990.109075","DOIUrl":null,"url":null,"abstract":"The basic operation principle of the TACAN navigation system on the Space Shuttle is described. An issue of interest to NASA engineers is the effect of the loss of the blanking pulse in the system. A simplified operation model of the shuttle TACAN receiver is presented. The effect is analyzed from the interference point of view in case of blanking pulse loss.<<ETX>>","PeriodicalId":141316,"journal":{"name":"IEEE Conference on Aerospace Applications","volume":"39 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1990-02-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Operation principle and loss of blanking pulse of the navigation system on Space Shuttle\",\"authors\":\"C. Tsang\",\"doi\":\"10.1109/AERO.1990.109075\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The basic operation principle of the TACAN navigation system on the Space Shuttle is described. An issue of interest to NASA engineers is the effect of the loss of the blanking pulse in the system. A simplified operation model of the shuttle TACAN receiver is presented. The effect is analyzed from the interference point of view in case of blanking pulse loss.<<ETX>>\",\"PeriodicalId\":141316,\"journal\":{\"name\":\"IEEE Conference on Aerospace Applications\",\"volume\":\"39 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1990-02-04\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Conference on Aerospace Applications\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO.1990.109075\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Conference on Aerospace Applications","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO.1990.109075","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Operation principle and loss of blanking pulse of the navigation system on Space Shuttle
The basic operation principle of the TACAN navigation system on the Space Shuttle is described. An issue of interest to NASA engineers is the effect of the loss of the blanking pulse in the system. A simplified operation model of the shuttle TACAN receiver is presented. The effect is analyzed from the interference point of view in case of blanking pulse loss.<>