{"title":"大型柔性航天器姿态控制系统设计","authors":"A. Nebylov, A. Panferov, S. Brodsky","doi":"10.31799/978-5-8088-1554-4-2021-2-223-227","DOIUrl":null,"url":null,"abstract":"The issues of control of a large space tug, consisting of a powerful power unit, an engine and automation unit remote from it, are considered. The blocks are connected by a long beam of about 50 m. Control of such a spacecraft (SC) is complicated by the considerable flexibility and elasticity of the beam and the significant weight of the blocks attached to it. The article discusses the issues of controlling the orientation of such a spacecraft and damping of the elastic oscillations.","PeriodicalId":318959,"journal":{"name":"The Second International Scientific Conference. Collection of reports","volume":"96 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-04-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"ATTITUDE CONTROL SYSTEMS DESIGN FOR A LARGE FLEXIBLE SPACECRAFT\",\"authors\":\"A. Nebylov, A. Panferov, S. Brodsky\",\"doi\":\"10.31799/978-5-8088-1554-4-2021-2-223-227\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The issues of control of a large space tug, consisting of a powerful power unit, an engine and automation unit remote from it, are considered. The blocks are connected by a long beam of about 50 m. Control of such a spacecraft (SC) is complicated by the considerable flexibility and elasticity of the beam and the significant weight of the blocks attached to it. The article discusses the issues of controlling the orientation of such a spacecraft and damping of the elastic oscillations.\",\"PeriodicalId\":318959,\"journal\":{\"name\":\"The Second International Scientific Conference. Collection of reports\",\"volume\":\"96 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-04-14\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"The Second International Scientific Conference. Collection of reports\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.31799/978-5-8088-1554-4-2021-2-223-227\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"The Second International Scientific Conference. Collection of reports","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.31799/978-5-8088-1554-4-2021-2-223-227","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
ATTITUDE CONTROL SYSTEMS DESIGN FOR A LARGE FLEXIBLE SPACECRAFT
The issues of control of a large space tug, consisting of a powerful power unit, an engine and automation unit remote from it, are considered. The blocks are connected by a long beam of about 50 m. Control of such a spacecraft (SC) is complicated by the considerable flexibility and elasticity of the beam and the significant weight of the blocks attached to it. The article discusses the issues of controlling the orientation of such a spacecraft and damping of the elastic oscillations.
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