{"title":"运动学GPS着陆系统架构及飞行试验结果","authors":"S. Cobb, C. Cohen, B. Parkinson","doi":"10.1109/NTC.1994.316683","DOIUrl":null,"url":null,"abstract":"Summary form only given, as follows. The kinematic GPS landing system (KGLS) uses differential GPS carrier phase data to navigate landing aircraft. As the aircraft overflies a \"GPS marker beacon\" during its approach, the KGLS sensor uses beacon data to resolve the carrier phase integer ambiguity. This deterministic method provides centimeter-level accuracy and high reliability on every approach.<<ETX>>","PeriodicalId":297184,"journal":{"name":"Proceedings of IEEE National Telesystems Conference - NTC '94","volume":"83 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1994-05-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Kinematic GPS landing system architecture and flight test results\",\"authors\":\"S. Cobb, C. Cohen, B. Parkinson\",\"doi\":\"10.1109/NTC.1994.316683\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Summary form only given, as follows. The kinematic GPS landing system (KGLS) uses differential GPS carrier phase data to navigate landing aircraft. As the aircraft overflies a \\\"GPS marker beacon\\\" during its approach, the KGLS sensor uses beacon data to resolve the carrier phase integer ambiguity. This deterministic method provides centimeter-level accuracy and high reliability on every approach.<<ETX>>\",\"PeriodicalId\":297184,\"journal\":{\"name\":\"Proceedings of IEEE National Telesystems Conference - NTC '94\",\"volume\":\"83 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1994-05-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of IEEE National Telesystems Conference - NTC '94\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/NTC.1994.316683\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of IEEE National Telesystems Conference - NTC '94","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/NTC.1994.316683","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Kinematic GPS landing system architecture and flight test results
Summary form only given, as follows. The kinematic GPS landing system (KGLS) uses differential GPS carrier phase data to navigate landing aircraft. As the aircraft overflies a "GPS marker beacon" during its approach, the KGLS sensor uses beacon data to resolve the carrier phase integer ambiguity. This deterministic method provides centimeter-level accuracy and high reliability on every approach.<>
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