{"title":"A Computer Simulation For A Space-Time Satellite Positioning System","authors":"J. Huntley, D. Tepper","doi":"10.1109/SIMSYM.1990.717280","DOIUrl":null,"url":null,"abstract":"This paper concerns the development of an autonomously distributed satellite network synchronization and positioning system. A simulation is developed to study the problem of having the member satellites obtain a system wide space-time coordinate reference system. The simulation models on board clocks for a system of satellites together with transfer via line of sight transmission using an EM signal of time and position data. It accounts for the various errors of measurement together with orbit mechanics that includes relativistic effects. Each satellite keeps a record of the defining equations for the orbits of the other members of the system. The ideal of the simulation is to find an algorithm for transferring timing and postion data that will produce much agreement as possible for these records for all the members of the system.","PeriodicalId":399502,"journal":{"name":"1990 Eastern Multiconference. Record of Proceedings. The 23rd Annual Simulation Symposium","volume":"231 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1990-04-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"1990 Eastern Multiconference. Record of Proceedings. The 23rd Annual Simulation Symposium","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/SIMSYM.1990.717280","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2
Abstract
This paper concerns the development of an autonomously distributed satellite network synchronization and positioning system. A simulation is developed to study the problem of having the member satellites obtain a system wide space-time coordinate reference system. The simulation models on board clocks for a system of satellites together with transfer via line of sight transmission using an EM signal of time and position data. It accounts for the various errors of measurement together with orbit mechanics that includes relativistic effects. Each satellite keeps a record of the defining equations for the orbits of the other members of the system. The ideal of the simulation is to find an algorithm for transferring timing and postion data that will produce much agreement as possible for these records for all the members of the system.