{"title":"装有太阳帆并系在日心空间站上的航天器的钟摆运动","authors":"A. V. Rodnikov","doi":"10.1109/STAB49150.2020.9140618","DOIUrl":null,"url":null,"abstract":"Motions of a spacecraft equipped with a solar sail and tethered to a heliocentric station is considered. The problems of the spacecraft motion along plane sections of a sphere, restricting its motion with respect to the station, are studied as analogs of perturbed librations of a spherical pendulum or as some generalizations of them.","PeriodicalId":166223,"journal":{"name":"2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference) (STAB)","volume":"44 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Pendulum Motions of a Spacecraft Equipped with a Solar Sail and Tethered to a Heliocentric Space Station\",\"authors\":\"A. V. Rodnikov\",\"doi\":\"10.1109/STAB49150.2020.9140618\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Motions of a spacecraft equipped with a solar sail and tethered to a heliocentric station is considered. The problems of the spacecraft motion along plane sections of a sphere, restricting its motion with respect to the station, are studied as analogs of perturbed librations of a spherical pendulum or as some generalizations of them.\",\"PeriodicalId\":166223,\"journal\":{\"name\":\"2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference) (STAB)\",\"volume\":\"44 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2020-06-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference) (STAB)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/STAB49150.2020.9140618\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference) (STAB)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/STAB49150.2020.9140618","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Pendulum Motions of a Spacecraft Equipped with a Solar Sail and Tethered to a Heliocentric Space Station
Motions of a spacecraft equipped with a solar sail and tethered to a heliocentric station is considered. The problems of the spacecraft motion along plane sections of a sphere, restricting its motion with respect to the station, are studied as analogs of perturbed librations of a spherical pendulum or as some generalizations of them.