{"title":"I类LAAS的轨道星历监测仪","authors":"L. Gratton, B. Pervan, S. Pullen","doi":"10.1109/PLANS.2004.1309026","DOIUrl":null,"url":null,"abstract":"This paper describes sufficient methodologies to monitor GPS satellite orbit ephemeris for Category I aircraft precision approach navigation. In the absence of a satellite maneuver, it is shown that a monitor based on the projection of previously validated ephemeris parameters is adequate to meet navigation integrity and availability requirements. After scheduled stationkeeping maneuvers, no previously validated ephemerides are available, so a measurement-based method is required. The feasibility of such a monitor is also established.","PeriodicalId":102388,"journal":{"name":"PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556)","volume":"108 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2004-04-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"9","resultStr":"{\"title\":\"Orbit ephemeris monitors for category I LAAS\",\"authors\":\"L. Gratton, B. Pervan, S. Pullen\",\"doi\":\"10.1109/PLANS.2004.1309026\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper describes sufficient methodologies to monitor GPS satellite orbit ephemeris for Category I aircraft precision approach navigation. In the absence of a satellite maneuver, it is shown that a monitor based on the projection of previously validated ephemeris parameters is adequate to meet navigation integrity and availability requirements. After scheduled stationkeeping maneuvers, no previously validated ephemerides are available, so a measurement-based method is required. The feasibility of such a monitor is also established.\",\"PeriodicalId\":102388,\"journal\":{\"name\":\"PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556)\",\"volume\":\"108 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2004-04-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"9\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/PLANS.2004.1309026\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/PLANS.2004.1309026","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
This paper describes sufficient methodologies to monitor GPS satellite orbit ephemeris for Category I aircraft precision approach navigation. In the absence of a satellite maneuver, it is shown that a monitor based on the projection of previously validated ephemeris parameters is adequate to meet navigation integrity and availability requirements. After scheduled stationkeeping maneuvers, no previously validated ephemerides are available, so a measurement-based method is required. The feasibility of such a monitor is also established.