{"title":"民航飞机惯性卫星集成系统发展展望","authors":"V. Sineglazov, F. M. Zaharin","doi":"10.1109/MSNMC.2012.6475074","DOIUrl":null,"url":null,"abstract":"Using an inertial navigation system and Global Positioning System together is preferable to using any of them separately. Derived benefits depend on the level of combining information. Inertial navigation systems/ Global Positioning System integration architectures are defined as separate, loosely and tightly coupled, deeply integrated configurations.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"35 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":"{\"title\":\"Perspectives of integrated inertial-satellite systems development of civil aviation aircraft\",\"authors\":\"V. Sineglazov, F. M. Zaharin\",\"doi\":\"10.1109/MSNMC.2012.6475074\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Using an inertial navigation system and Global Positioning System together is preferable to using any of them separately. Derived benefits depend on the level of combining information. Inertial navigation systems/ Global Positioning System integration architectures are defined as separate, loosely and tightly coupled, deeply integrated configurations.\",\"PeriodicalId\":394899,\"journal\":{\"name\":\"2012 2nd International Conference \\\"Methods and Systems of Navigation and Motion Control\\\" (MSNMC)\",\"volume\":\"35 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2012-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"3\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2012 2nd International Conference \\\"Methods and Systems of Navigation and Motion Control\\\" (MSNMC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/MSNMC.2012.6475074\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MSNMC.2012.6475074","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Perspectives of integrated inertial-satellite systems development of civil aviation aircraft
Using an inertial navigation system and Global Positioning System together is preferable to using any of them separately. Derived benefits depend on the level of combining information. Inertial navigation systems/ Global Positioning System integration architectures are defined as separate, loosely and tightly coupled, deeply integrated configurations.