{"title":"GPS/INS integration for civil aviation","authors":"J. Diesel","doi":"10.1109/NTC.1991.148022","DOIUrl":null,"url":null,"abstract":"The mechanization equations for generating the INS (inertial navigation system) solution in the proper coordinates are presented. Two different Kalman filter error models for integrating GPS (Global Positioning System) with INS are derived. The model which uses spheroidal component differences rather than Cartesian vector differences is preferable, since it uses error states which can be directly corrected in the INS mechanization equations.<<ETX>>","PeriodicalId":320008,"journal":{"name":"NTC '91 - National Telesystems Conference Proceedings","volume":"27 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1991-03-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"11","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"NTC '91 - National Telesystems Conference Proceedings","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/NTC.1991.148022","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 11
Abstract
The mechanization equations for generating the INS (inertial navigation system) solution in the proper coordinates are presented. Two different Kalman filter error models for integrating GPS (Global Positioning System) with INS are derived. The model which uses spheroidal component differences rather than Cartesian vector differences is preferable, since it uses error states which can be directly corrected in the INS mechanization equations.<>
京公网安备 11010802042870号
京ICP备2023020795号-1
分享
求助内容：
应助结果提醒方式：
扫码关注我们
