{"title":"一对纳米卫星编队飞行控制分析","authors":"S. Veres, Stephen B. Gabriel, E. Rogers, D. Mayne","doi":"10.1109/CDC.2001.981031","DOIUrl":null,"url":null,"abstract":"Gives an analysis and provides implementable solutions for constrained control problems of stabilization and maneuver control of two nano-satellites. The methodology provides solutions under various constraints of propulsion and differential drag control: magnitude constraints, disturbances and measurement errors are taken into account. The methods are illustrated in simulation of a realistic nano-satellite pair.","PeriodicalId":131411,"journal":{"name":"Proceedings of the 40th IEEE Conference on Decision and Control (Cat. No.01CH37228)","volume":"20 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2001-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"23","resultStr":"{\"title\":\"Analysis of formation flying control of a pair of nano-satellites\",\"authors\":\"S. Veres, Stephen B. Gabriel, E. Rogers, D. Mayne\",\"doi\":\"10.1109/CDC.2001.981031\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Gives an analysis and provides implementable solutions for constrained control problems of stabilization and maneuver control of two nano-satellites. The methodology provides solutions under various constraints of propulsion and differential drag control: magnitude constraints, disturbances and measurement errors are taken into account. The methods are illustrated in simulation of a realistic nano-satellite pair.\",\"PeriodicalId\":131411,\"journal\":{\"name\":\"Proceedings of the 40th IEEE Conference on Decision and Control (Cat. No.01CH37228)\",\"volume\":\"20 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2001-12-04\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"23\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the 40th IEEE Conference on Decision and Control (Cat. No.01CH37228)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CDC.2001.981031\",\"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 40th IEEE Conference on Decision and Control (Cat. No.01CH37228)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CDC.2001.981031","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Analysis of formation flying control of a pair of nano-satellites
Gives an analysis and provides implementable solutions for constrained control problems of stabilization and maneuver control of two nano-satellites. The methodology provides solutions under various constraints of propulsion and differential drag control: magnitude constraints, disturbances and measurement errors are taken into account. The methods are illustrated in simulation of a realistic nano-satellite pair.
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