Electric Thrusters Configuration Strategy Study on Station-Keeping and Momentum Dumping of GEO Satellite

2019 5th International Conference on Control Science and Systems Engineering (ICCSSE) Pub Date : 2019-08-01 DOI:10.1109/ICCSSE.2019.00030

Wang Min, Li Qiang, Liang Xingang, An Ran

{"title":"Electric Thrusters Configuration Strategy Study on Station-Keeping and Momentum Dumping of GEO Satellite","authors":"Wang Min, Li Qiang, Liang Xingang, An Ran","doi":"10.1109/ICCSSE.2019.00030","DOIUrl":null,"url":null,"abstract":"More and more GEO Satellites adopts electric thrusters to execute station-keeping and momentum dumping. Profiting from the high specific impulse of electric propulsion, there is substantially decrease in fuel consumption and improvement in payload capacity. Quantity and configuration of electric thrusters have a large influence in station-keeping efficiency and momentum dumping capacity. Considering the necessary of system backup, the station-keeping and momentum dumping must be performed correctly while at least one thruster breaks down. In this paper, a method of station-keeping and momentum dumping capacity analysis is introduced, from which the minimum configuration of electric thrusters is induced. In addition, the minimum configuration of electric thrusters for GEO satellite station-keeping and momentum dumping with backup is discussed. At last, the relationship between thrusters' installation parameters and capacity of station-keeping and momentum dumping is analyzed. In view of the above, the designing method of electric thrusters' installation parameters is obtained.","PeriodicalId":443482,"journal":{"name":"2019 5th International Conference on Control Science and Systems Engineering (ICCSSE)","volume":"11 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 5th International Conference on Control Science and Systems Engineering (ICCSSE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICCSSE.2019.00030","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 1

Abstract

More and more GEO Satellites adopts electric thrusters to execute station-keeping and momentum dumping. Profiting from the high specific impulse of electric propulsion, there is substantially decrease in fuel consumption and improvement in payload capacity. Quantity and configuration of electric thrusters have a large influence in station-keeping efficiency and momentum dumping capacity. Considering the necessary of system backup, the station-keeping and momentum dumping must be performed correctly while at least one thruster breaks down. In this paper, a method of station-keeping and momentum dumping capacity analysis is introduced, from which the minimum configuration of electric thrusters is induced. In addition, the minimum configuration of electric thrusters for GEO satellite station-keeping and momentum dumping with backup is discussed. At last, the relationship between thrusters' installation parameters and capacity of station-keeping and momentum dumping is analyzed. In view of the above, the designing method of electric thrusters' installation parameters is obtained.

查看原文本刊更多论文

地球同步轨道卫星保持站位和动量倾倒的电动推进器配置策略研究

越来越多的地球同步轨道卫星采用电动推力器进行站位保持和动量倾倒。得益于电力推进的高比冲，大大降低了燃料消耗，提高了有效载荷能力。电动推力器的数量和配置对电站保持效率和动量倾倒能力有很大的影响。考虑到系统备份的必要性，在至少一个推进器发生故障的情况下，必须正确进行站位保持和动量倾倒。本文介绍了一种站位保持和动量倾倒能力分析的方法，并由此导出了电动推进器的最小配置。此外，还讨论了地球同步轨道卫星保持站和备用动量倾倒的最小配置。最后，分析了推力器安装参数与保持站位和动量倾倒能力的关系。由此得出了电动推进器安装参数的设计方法。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

求助全文

约1分钟内获得全文求助全文

来源期刊

2019 5th International Conference on Control Science and Systems Engineering (ICCSSE)

自引率

0.00%

发文量