{"title":"高椭圆轨道卫星重力梯度姿态控制系统","authors":"M. Ovchinnikov, A. Dyachenko","doi":"10.1109/ICSC.1996.864254","DOIUrl":null,"url":null,"abstract":"In this paper we deal with stationary and periodic motions of satellites in elliptical orbits, including the high eccentricity case, which motions can serve as nominal for satellites with passive attitude control system. We analyze the possibility of using resonance motions of satellites in the Earth's gravity and magnetic fields to comply with the required amplitude characteristics and stability of these solutions under effecting an eddy current damper.","PeriodicalId":154434,"journal":{"name":"Proceedings of The 2nd International Conference on Satellite Communications","volume":"25 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1996-09-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":"{\"title\":\"Gravity-gradient attitude control systems for a satellite on a high-elliptical orbits\",\"authors\":\"M. Ovchinnikov, A. Dyachenko\",\"doi\":\"10.1109/ICSC.1996.864254\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper we deal with stationary and periodic motions of satellites in elliptical orbits, including the high eccentricity case, which motions can serve as nominal for satellites with passive attitude control system. We analyze the possibility of using resonance motions of satellites in the Earth's gravity and magnetic fields to comply with the required amplitude characteristics and stability of these solutions under effecting an eddy current damper.\",\"PeriodicalId\":154434,\"journal\":{\"name\":\"Proceedings of The 2nd International Conference on Satellite Communications\",\"volume\":\"25 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1996-09-23\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"4\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of The 2nd International Conference on Satellite Communications\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICSC.1996.864254\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of The 2nd International Conference on Satellite Communications","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICSC.1996.864254","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Gravity-gradient attitude control systems for a satellite on a high-elliptical orbits
In this paper we deal with stationary and periodic motions of satellites in elliptical orbits, including the high eccentricity case, which motions can serve as nominal for satellites with passive attitude control system. We analyze the possibility of using resonance motions of satellites in the Earth's gravity and magnetic fields to comply with the required amplitude characteristics and stability of these solutions under effecting an eddy current damper.
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