基于联邦滤波器的微纳卫星测量算法研究

Yuanming Ding, Huaxian Chen, Ran Zhang
{"title":"基于联邦滤波器的微纳卫星测量算法研究","authors":"Yuanming Ding, Huaxian Chen, Ran Zhang","doi":"10.1109/ICMRA51221.2020.9398333","DOIUrl":null,"url":null,"abstract":"In order to determine the position and speed of the main satellite in the micro-nano satellite formation, this paper proposes a micro-nano satellite measurement algorithm based on federal filter. First, three-axis magnetometer and magnetoresistive sensor are used to measure the position and speed of the main satellite due to the uncertainty of the distribution of the geomagnetic field. Since in the place where the earth's magnetic field changes relatively, the sudden change of the satellite state will be obvious, then the strong tracking filter and the particle filter are used to solve the sudden change in the satellite motion and the low precision. Finally, the information fusion method is used to combine multiple filters to improve the performance. The simulation results show that the proposed measurement method can not only track the state of the satellite in real time, but also reduce the measurement error and achieve accurate measurement.","PeriodicalId":160127,"journal":{"name":"2020 3rd International Conference on Mechatronics, Robotics and Automation (ICMRA)","volume":"124 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-10-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Research on Micro-Nano Satellite Measurement Algorithm Based on Federal Filter\",\"authors\":\"Yuanming Ding, Huaxian Chen, Ran Zhang\",\"doi\":\"10.1109/ICMRA51221.2020.9398333\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In order to determine the position and speed of the main satellite in the micro-nano satellite formation, this paper proposes a micro-nano satellite measurement algorithm based on federal filter. First, three-axis magnetometer and magnetoresistive sensor are used to measure the position and speed of the main satellite due to the uncertainty of the distribution of the geomagnetic field. Since in the place where the earth's magnetic field changes relatively, the sudden change of the satellite state will be obvious, then the strong tracking filter and the particle filter are used to solve the sudden change in the satellite motion and the low precision. Finally, the information fusion method is used to combine multiple filters to improve the performance. The simulation results show that the proposed measurement method can not only track the state of the satellite in real time, but also reduce the measurement error and achieve accurate measurement.\",\"PeriodicalId\":160127,\"journal\":{\"name\":\"2020 3rd International Conference on Mechatronics, Robotics and Automation (ICMRA)\",\"volume\":\"124 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2020-10-16\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2020 3rd International Conference on Mechatronics, Robotics and Automation (ICMRA)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICMRA51221.2020.9398333\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 3rd International Conference on Mechatronics, Robotics and Automation (ICMRA)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICMRA51221.2020.9398333","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

为了确定微纳卫星编队中主卫星的位置和速度,本文提出了一种基于联邦滤波器的微纳卫星测量算法。首先,由于地磁场分布的不确定性,采用三轴磁强计和磁阻传感器测量主卫星的位置和速度;由于在地磁场变化相对较大的地方,卫星状态的突变会比较明显,因此采用强跟踪滤波和粒子滤波来解决卫星运动的突变和精度较低的问题。最后,采用信息融合的方法将多个滤波器组合在一起,提高了性能。仿真结果表明,该测量方法既能实时跟踪卫星的状态,又能减小测量误差,实现精确测量。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Research on Micro-Nano Satellite Measurement Algorithm Based on Federal Filter
In order to determine the position and speed of the main satellite in the micro-nano satellite formation, this paper proposes a micro-nano satellite measurement algorithm based on federal filter. First, three-axis magnetometer and magnetoresistive sensor are used to measure the position and speed of the main satellite due to the uncertainty of the distribution of the geomagnetic field. Since in the place where the earth's magnetic field changes relatively, the sudden change of the satellite state will be obvious, then the strong tracking filter and the particle filter are used to solve the sudden change in the satellite motion and the low precision. Finally, the information fusion method is used to combine multiple filters to improve the performance. The simulation results show that the proposed measurement method can not only track the state of the satellite in real time, but also reduce the measurement error and achieve accurate measurement.
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