“Bankir”卫星通信和数据传输系统的“KUPON”飞船

S.D. Koulikov, K.M. Pitchkhadze, V. Makarov, V. Kouznetsov
{"title":"“Bankir”卫星通信和数据传输系统的“KUPON”飞船","authors":"S.D. Koulikov, K.M. Pitchkhadze, V. Makarov, V. Kouznetsov","doi":"10.1109/ICSC.1998.741343","DOIUrl":null,"url":null,"abstract":"The \"KUPON\" spacecraft is designed for data retranslation (data transmission, telefax, telephone) between subscribers of the satellite communication network. It was developed for the \"Bankir\" satellite communication and data transmitting system of the Central Bank of Russian Federation. The spacecraft was designed on the basis of the Lavochkin satellite communications. That has led to a decrease in terms of development and tests, cost of the spacecrafts and the entire communication system as well. The covering zone is formed by three S/C of the orbital system, each of them having on-board retranslation complexes (BRTK) working in Ku-band (14/11 GHz). Active phased antenna grids (AFAR) that can form up to 16 narrow receiving-transmitting beams, that can be retargeted to any undersatellite point in the limit of the S/C viewing area, are used, giving a possibility of changing the covering zones in the limits of the viewing area and to have flexible redistribution of the retranslator working ability. S/C injection into the staying points is performed by the three-staged \"Proton\" launch vehicle with the upper stage \"DM\" from the Baikonour launch site. In order to solve tasks of the on-board systems and also to perform control, diagnostics and recovery of the on-board systems, there is an on-board control complex (BKU), and in order to provide normal functioning of the BKU and BRTK for the execution of the input before the S/C tasks, there is an on-board control complex of service systems (BKOS).","PeriodicalId":240115,"journal":{"name":"3rd International Conference on Satellite Communications (IEEE Cat. No.98TH8392)","volume":"25 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1998-09-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"\\\"KUPON\\\" spacecraft of \\\"Bankir\\\" satellite communication and data transmitting system\",\"authors\":\"S.D. Koulikov, K.M. Pitchkhadze, V. Makarov, V. Kouznetsov\",\"doi\":\"10.1109/ICSC.1998.741343\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The \\\"KUPON\\\" spacecraft is designed for data retranslation (data transmission, telefax, telephone) between subscribers of the satellite communication network. It was developed for the \\\"Bankir\\\" satellite communication and data transmitting system of the Central Bank of Russian Federation. The spacecraft was designed on the basis of the Lavochkin satellite communications. That has led to a decrease in terms of development and tests, cost of the spacecrafts and the entire communication system as well. The covering zone is formed by three S/C of the orbital system, each of them having on-board retranslation complexes (BRTK) working in Ku-band (14/11 GHz). Active phased antenna grids (AFAR) that can form up to 16 narrow receiving-transmitting beams, that can be retargeted to any undersatellite point in the limit of the S/C viewing area, are used, giving a possibility of changing the covering zones in the limits of the viewing area and to have flexible redistribution of the retranslator working ability. S/C injection into the staying points is performed by the three-staged \\\"Proton\\\" launch vehicle with the upper stage \\\"DM\\\" from the Baikonour launch site. In order to solve tasks of the on-board systems and also to perform control, diagnostics and recovery of the on-board systems, there is an on-board control complex (BKU), and in order to provide normal functioning of the BKU and BRTK for the execution of the input before the S/C tasks, there is an on-board control complex of service systems (BKOS).\",\"PeriodicalId\":240115,\"journal\":{\"name\":\"3rd International Conference on Satellite Communications (IEEE Cat. No.98TH8392)\",\"volume\":\"25 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1998-09-22\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"3rd International Conference on Satellite Communications (IEEE Cat. No.98TH8392)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICSC.1998.741343\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"3rd International Conference on Satellite Communications (IEEE Cat. No.98TH8392)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICSC.1998.741343","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

摘要

“KUPON”航天器设计用于卫星通信网络用户之间的数据转译(数据传输、电传、电话)。它是为俄罗斯联邦中央银行的“Bankir”卫星通信和数据传输系统开发的。该航天器是在拉沃奇金卫星通信的基础上设计的。这导致了开发和测试方面的减少,航天器和整个通信系统的成本也减少了。覆盖区由轨道系统的三个S/C组成,每个S/C都有工作在ku波段(14/11 GHz)的星载转译复合物(BRTK)。采用最多可形成16个窄波束的有源相控天线栅格(AFAR),可将其重定向到S/C观测区域极限内的任何星下点,从而提供了在观测区域极限内改变覆盖区域的可能性,并具有灵活地重新分配转转换器工作能力。S/C注入停留点是由三级“质子”运载火箭在拜科努尔发射场进行的,上面一级是“DM”。为了解决车载系统的任务,也为了执行车载系统的控制、诊断和恢复,有一个车载控制综合体(BKU),为了提供BKU和BRTK的正常功能,以执行S/C任务之前的输入,有一个车载控制服务系统综合体(BKOS)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
"KUPON" spacecraft of "Bankir" satellite communication and data transmitting system
The "KUPON" spacecraft is designed for data retranslation (data transmission, telefax, telephone) between subscribers of the satellite communication network. It was developed for the "Bankir" satellite communication and data transmitting system of the Central Bank of Russian Federation. The spacecraft was designed on the basis of the Lavochkin satellite communications. That has led to a decrease in terms of development and tests, cost of the spacecrafts and the entire communication system as well. The covering zone is formed by three S/C of the orbital system, each of them having on-board retranslation complexes (BRTK) working in Ku-band (14/11 GHz). Active phased antenna grids (AFAR) that can form up to 16 narrow receiving-transmitting beams, that can be retargeted to any undersatellite point in the limit of the S/C viewing area, are used, giving a possibility of changing the covering zones in the limits of the viewing area and to have flexible redistribution of the retranslator working ability. S/C injection into the staying points is performed by the three-staged "Proton" launch vehicle with the upper stage "DM" from the Baikonour launch site. In order to solve tasks of the on-board systems and also to perform control, diagnostics and recovery of the on-board systems, there is an on-board control complex (BKU), and in order to provide normal functioning of the BKU and BRTK for the execution of the input before the S/C tasks, there is an on-board control complex of service systems (BKOS).
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信