{"title":"矢量惯性导航原理","authors":"A. Schneider","doi":"10.1109/TANE3.1959.4201690","DOIUrl":null,"url":null,"abstract":"A vector equation, which is derived from first principles, describes the mechanization of inertial navigation systems for use anywhere in space. A specialized form of this equation applies directly to three-dimensional motion at any speed, any altitude, over an elliptical, rotating earth. The usefulness of this equation is illustrated by working out an example of a system design. Behavior of errors in inertial systems is also discussed.","PeriodicalId":332621,"journal":{"name":"IRE Transactions on Aeronautical and Navigational Electronics","volume":"ANE-6 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1959-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Vector Principles of Inertial Navigation\",\"authors\":\"A. Schneider\",\"doi\":\"10.1109/TANE3.1959.4201690\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A vector equation, which is derived from first principles, describes the mechanization of inertial navigation systems for use anywhere in space. A specialized form of this equation applies directly to three-dimensional motion at any speed, any altitude, over an elliptical, rotating earth. The usefulness of this equation is illustrated by working out an example of a system design. Behavior of errors in inertial systems is also discussed.\",\"PeriodicalId\":332621,\"journal\":{\"name\":\"IRE Transactions on Aeronautical and Navigational Electronics\",\"volume\":\"ANE-6 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1959-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IRE Transactions on Aeronautical and Navigational Electronics\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/TANE3.1959.4201690\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IRE Transactions on Aeronautical and Navigational Electronics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/TANE3.1959.4201690","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
A vector equation, which is derived from first principles, describes the mechanization of inertial navigation systems for use anywhere in space. A specialized form of this equation applies directly to three-dimensional motion at any speed, any altitude, over an elliptical, rotating earth. The usefulness of this equation is illustrated by working out an example of a system design. Behavior of errors in inertial systems is also discussed.
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