{"title":"鲁棒柔性航天器控制系统设计","authors":"F. Bauer, Ching-Fang Lin, Q. Liu, Qinghong Wang","doi":"10.1109/AEROCS.1993.720900","DOIUrl":null,"url":null,"abstract":"In this paper, varions robust control design methods are examined and their synergistic integration is investigated to meet the stringent performance and robustness requirements of flexible spacecraft. The robust control design methodologies are illustrated through the attitude control system design for the X-ray Timing Explorer satellite.","PeriodicalId":170527,"journal":{"name":"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,","volume":"217 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1993-05-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Robust Flexible Spacecraft Control System Design\",\"authors\":\"F. Bauer, Ching-Fang Lin, Q. Liu, Qinghong Wang\",\"doi\":\"10.1109/AEROCS.1993.720900\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper, varions robust control design methods are examined and their synergistic integration is investigated to meet the stringent performance and robustness requirements of flexible spacecraft. The robust control design methodologies are illustrated through the attitude control system design for the X-ray Timing Explorer satellite.\",\"PeriodicalId\":170527,\"journal\":{\"name\":\"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,\",\"volume\":\"217 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1993-05-25\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AEROCS.1993.720900\",\"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. The First IEEE Regional Conference on Aerospace Control Systems,","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AEROCS.1993.720900","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
In this paper, varions robust control design methods are examined and their synergistic integration is investigated to meet the stringent performance and robustness requirements of flexible spacecraft. The robust control design methodologies are illustrated through the attitude control system design for the X-ray Timing Explorer satellite.
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