{"title":"基于视频信息的测量卫星导航运动控制系统精度的飞行检验","authors":"Y. Somov, S. Butyrin, T. Somova, S. Somov","doi":"10.23919/ICINS.2019.8769408","DOIUrl":null,"url":null,"abstract":"Contemporary land-survey satellites are placed in the orbits with altitude of up to 1000 km. For such spacecraft we present the methods developed for in-flight verification of its attitude control system based on the analysis of an image motion in the onboard telescope during scanning optoelectronic imagery.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"117 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"In-flight Checking of the Accuracy of the Navigation and Motion Control System for a Surveying Satellite Using Video Information\",\"authors\":\"Y. Somov, S. Butyrin, T. Somova, S. Somov\",\"doi\":\"10.23919/ICINS.2019.8769408\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Contemporary land-survey satellites are placed in the orbits with altitude of up to 1000 km. For such spacecraft we present the methods developed for in-flight verification of its attitude control system based on the analysis of an image motion in the onboard telescope during scanning optoelectronic imagery.\",\"PeriodicalId\":108493,\"journal\":{\"name\":\"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)\",\"volume\":\"117 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2019-05-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23919/ICINS.2019.8769408\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/ICINS.2019.8769408","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
In-flight Checking of the Accuracy of the Navigation and Motion Control System for a Surveying Satellite Using Video Information
Contemporary land-survey satellites are placed in the orbits with altitude of up to 1000 km. For such spacecraft we present the methods developed for in-flight verification of its attitude control system based on the analysis of an image motion in the onboard telescope during scanning optoelectronic imagery.
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