{"title":"全球不间断卫星通信系统抛射参数优化","authors":"O. P. Nesterenko, E.M. Sabirov, M. S. Sergeev","doi":"10.1109/ICSC.1996.865387","DOIUrl":null,"url":null,"abstract":"Optimization of projectible parameters of global satellite-based mobile voice/data telephone service is considered. Such a global system must guarantee uninterrupted communication all over the world. Optimization criterion is total expenses of satellite segment deployment and its operation and maintenance. Basic input data is: performances of ground network segment and spatial density of users. The software for complex optimization is presented for following parameters: orbital structure , total satellite mass , performances of aboard transponder , power consumption and performances of correction engine. Additionally the launch vehicle options and possibility of cluster launch are taken into consideration.","PeriodicalId":154434,"journal":{"name":"Proceedings of The 2nd International Conference on Satellite Communications","volume":"33 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1996-09-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Optimization of projectible parameters of global uninterrupted satellite communication system\",\"authors\":\"O. P. Nesterenko, E.M. Sabirov, M. S. Sergeev\",\"doi\":\"10.1109/ICSC.1996.865387\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Optimization of projectible parameters of global satellite-based mobile voice/data telephone service is considered. Such a global system must guarantee uninterrupted communication all over the world. Optimization criterion is total expenses of satellite segment deployment and its operation and maintenance. Basic input data is: performances of ground network segment and spatial density of users. The software for complex optimization is presented for following parameters: orbital structure , total satellite mass , performances of aboard transponder , power consumption and performances of correction engine. Additionally the launch vehicle options and possibility of cluster launch are taken into consideration.\",\"PeriodicalId\":154434,\"journal\":{\"name\":\"Proceedings of The 2nd International Conference on Satellite Communications\",\"volume\":\"33 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.1996.865387\",\"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.1996.865387","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Optimization of projectible parameters of global uninterrupted satellite communication system
Optimization of projectible parameters of global satellite-based mobile voice/data telephone service is considered. Such a global system must guarantee uninterrupted communication all over the world. Optimization criterion is total expenses of satellite segment deployment and its operation and maintenance. Basic input data is: performances of ground network segment and spatial density of users. The software for complex optimization is presented for following parameters: orbital structure , total satellite mass , performances of aboard transponder , power consumption and performances of correction engine. Additionally the launch vehicle options and possibility of cluster launch are taken into consideration.
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