{"title":"卫星通信系统中航天器最优控制运动参数的确定","authors":"V.V. Betanov, O. A. Alekseev, V.G. Yashin","doi":"10.1109/ICSC.1996.864253","DOIUrl":null,"url":null,"abstract":"Special features of applying the method of fastest restoration of couplings to calculation of control parameters of spacecraft maneuvers are considered. Applkabillty of this method to various versions of maneuvers is analyzed. A modification of the parameter refinement procedure by introduction of weighting coefficients is investigated.","PeriodicalId":154434,"journal":{"name":"Proceedings of The 2nd International Conference on Satellite Communications","volume":"39 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1996-09-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Determination optimal control motion parameters of spacecraft in satellite communication systems\",\"authors\":\"V.V. Betanov, O. A. Alekseev, V.G. Yashin\",\"doi\":\"10.1109/ICSC.1996.864253\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Special features of applying the method of fastest restoration of couplings to calculation of control parameters of spacecraft maneuvers are considered. Applkabillty of this method to various versions of maneuvers is analyzed. A modification of the parameter refinement procedure by introduction of weighting coefficients is investigated.\",\"PeriodicalId\":154434,\"journal\":{\"name\":\"Proceedings of The 2nd International Conference on Satellite Communications\",\"volume\":\"39 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1996-09-23\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"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.1996.864253\",\"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.1996.864253","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Determination optimal control motion parameters of spacecraft in satellite communication systems
Special features of applying the method of fastest restoration of couplings to calculation of control parameters of spacecraft maneuvers are considered. Applkabillty of this method to various versions of maneuvers is analyzed. A modification of the parameter refinement procedure by introduction of weighting coefficients is investigated.