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The scheme of satellite navigation performance evaluation and test system based on simulation

  • Xiaojing Xia*
  • , Dong Xu
  • , Yan Zhao
  • *此作品的通讯作者
  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

A satellite navigation performance evaluation and test system framework structure based on simulation has been conceived and developed targeting the windows operating system, so as to extract and analyze he key performance of satellite navigation system The evaluation methods of Ionospheric model errors, Space vehicles (SVs) clock errors and Ephemeris prediction errors were presented. While testing physical receiver performance, the mathematical simulation satellite navigation subsystem except receiver was used to help. It can provide references for satellite navigation performance evaluation and test.

源语言英语
主期刊名Seventh International Symposium on Instrumentation and Control Technology
主期刊副标题Measurement Theory and Systems and Aeronautical Equipment
DOI
出版状态已出版 - 2008
活动7th International Symposium on Instrumentation and Control Technology: Measurement Theory and Systems and Aeronautical Equipment - Beijing, 中国
期限: 10 10月 200813 10月 2008

出版系列

姓名Proceedings of SPIE - The International Society for Optical Engineering
7128
ISSN(印刷版)0277-786X

会议

会议7th International Symposium on Instrumentation and Control Technology: Measurement Theory and Systems and Aeronautical Equipment
国家/地区中国
Beijing
时期10/10/0813/10/08

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