{"title":"机动陆地测量卫星的精确天文惯性姿态测定","authors":"Y. Somov, S. Butyrin, S. Somov, C. Hajiyev","doi":"10.1109/RAST.2017.8003010","DOIUrl":null,"url":null,"abstract":"We consider some principal problems on precise attitude determination of the maneuvering land-survey satellites placed on the orbit altitudes from 600 up to 1000 km. We present onboard discrete algorithms for signal processing, calibration and alignment of astroinertial attitude determination system which is a part of the strapdown inertial navigation system.","PeriodicalId":434418,"journal":{"name":"2017 8th International Conference on Recent Advances in Space Technologies (RAST)","volume":"182 ","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"10","resultStr":"{\"title\":\"Precise astroinertial attitude determination of a maneuvering land-survey satellite\",\"authors\":\"Y. Somov, S. Butyrin, S. Somov, C. Hajiyev\",\"doi\":\"10.1109/RAST.2017.8003010\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"We consider some principal problems on precise attitude determination of the maneuvering land-survey satellites placed on the orbit altitudes from 600 up to 1000 km. We present onboard discrete algorithms for signal processing, calibration and alignment of astroinertial attitude determination system which is a part of the strapdown inertial navigation system.\",\"PeriodicalId\":434418,\"journal\":{\"name\":\"2017 8th International Conference on Recent Advances in Space Technologies (RAST)\",\"volume\":\"182 \",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"10\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2017 8th International Conference on Recent Advances in Space Technologies (RAST)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/RAST.2017.8003010\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 8th International Conference on Recent Advances in Space Technologies (RAST)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/RAST.2017.8003010","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Precise astroinertial attitude determination of a maneuvering land-survey satellite
We consider some principal problems on precise attitude determination of the maneuvering land-survey satellites placed on the orbit altitudes from 600 up to 1000 km. We present onboard discrete algorithms for signal processing, calibration and alignment of astroinertial attitude determination system which is a part of the strapdown inertial navigation system.