{"title":"圆形轨道重力阻尼复合纳米卫星姿态动力学研究","authors":"A. Doroshin, A. Eremenko","doi":"10.1109/ITNT57377.2023.10139197","DOIUrl":null,"url":null,"abstract":"The paper considers the attitude dynamics of a composite nanosatellite on circular orbits. The nanosatellite consists of two modules - a carrier body and a movable unit. The carrier body contains a gravitational damper. Into the movable unit a flywheel engine is installed, and the angular velocity of its rotor is constant. The mathematical model of attitude motion is built, and the numerical study of the dynamics is carried out.","PeriodicalId":296438,"journal":{"name":"2023 IX International Conference on Information Technology and Nanotechnology (ITNT)","volume":"88 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2023-04-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Investigation of the attitude dynamics of a composite nanosatellite with a gravitational damper on circular orbits\",\"authors\":\"A. Doroshin, A. Eremenko\",\"doi\":\"10.1109/ITNT57377.2023.10139197\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The paper considers the attitude dynamics of a composite nanosatellite on circular orbits. The nanosatellite consists of two modules - a carrier body and a movable unit. The carrier body contains a gravitational damper. Into the movable unit a flywheel engine is installed, and the angular velocity of its rotor is constant. The mathematical model of attitude motion is built, and the numerical study of the dynamics is carried out.\",\"PeriodicalId\":296438,\"journal\":{\"name\":\"2023 IX International Conference on Information Technology and Nanotechnology (ITNT)\",\"volume\":\"88 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2023-04-17\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2023 IX International Conference on Information Technology and Nanotechnology (ITNT)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ITNT57377.2023.10139197\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2023 IX International Conference on Information Technology and Nanotechnology (ITNT)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ITNT57377.2023.10139197","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Investigation of the attitude dynamics of a composite nanosatellite with a gravitational damper on circular orbits
The paper considers the attitude dynamics of a composite nanosatellite on circular orbits. The nanosatellite consists of two modules - a carrier body and a movable unit. The carrier body contains a gravitational damper. Into the movable unit a flywheel engine is installed, and the angular velocity of its rotor is constant. The mathematical model of attitude motion is built, and the numerical study of the dynamics is carried out.
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