{"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}
引用次数: 0
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.<>
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