基于GNSS技术的无线电罗盘估计纳米卫星惯性特性

2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI:10.23919/ICINS.2019.8769358

A. Kramlikh, I. Lomaka, S. Shafran

{"title":"基于GNSS技术的无线电罗盘估计纳米卫星惯性特性","authors":"A. Kramlikh, I. Lomaka, S. Shafran","doi":"10.23919/ICINS.2019.8769358","DOIUrl":null,"url":null,"abstract":"The paper describes a radio compass based on GNSS technology, an algorithm for processing GNSS information, an algorithm for calculating the coordinates of a unit vector of the longitudinal axis of a nanosatellite, and an approach that allows an estimation of the inertial characteristics of a nanosatellite. The estimation of the influence of the baseline length on the accuracy of determining the orientation angles is given. The results of the statistical study of the error determination of the nanosatellite inertial parameters using a radio compass are presented.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Estimating the Inertial Characteristics of a Nanosatellite Using a Radio Compass Based on GNSS Technology\",\"authors\":\"A. Kramlikh, I. Lomaka, S. Shafran\",\"doi\":\"10.23919/ICINS.2019.8769358\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The paper describes a radio compass based on GNSS technology, an algorithm for processing GNSS information, an algorithm for calculating the coordinates of a unit vector of the longitudinal axis of a nanosatellite, and an approach that allows an estimation of the inertial characteristics of a nanosatellite. The estimation of the influence of the baseline length on the accuracy of determining the orientation angles is given. The results of the statistical study of the error determination of the nanosatellite inertial parameters using a radio compass are presented.\",\"PeriodicalId\":108493,\"journal\":{\"name\":\"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2019-05-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23919/ICINS.2019.8769358\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/ICINS.2019.8769358","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 1

摘要

本文介绍了一种基于GNSS技术的无线电罗盘、GNSS信息处理算法、纳米卫星纵轴单位矢量坐标计算算法以及纳米卫星惯性特性估计方法。给出了基线长度对确定定向角精度的影响估计。给出了利用无线电罗盘测定纳米卫星惯性参数误差的统计研究结果。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Estimating the Inertial Characteristics of a Nanosatellite Using a Radio Compass Based on GNSS Technology

The paper describes a radio compass based on GNSS technology, an algorithm for processing GNSS information, an algorithm for calculating the coordinates of a unit vector of the longitudinal axis of a nanosatellite, and an approach that allows an estimation of the inertial characteristics of a nanosatellite. The estimation of the influence of the baseline length on the accuracy of determining the orientation angles is given. The results of the statistical study of the error determination of the nanosatellite inertial parameters using a radio compass are presented.

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

2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)

自引率

0.00%

发文量