我国GEO卫星高精度测定轨技术进展  被引量:4

Evolution of High-precision Orbit Determination Technology of GEO Satellite in China

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作  者:耿虎军[1] 刘友永[1] 王彬[1] 高华宇[1] GENG Hujun;LIU Youyong;WANG Bin;GAO Huayu(The 54th Research Institute of CETC,Shijiazhuang 050081,China)

机构地区:[1]中国电子科技集团公司第五十四研究所,河北石家庄050081

出  处:《无线电工程》2019年第5期357-362,共6页Radio Engineering

基  金:中国电子科技集团公司航天信息应用技术重点实验室开放基金资助项目(SXX18629T022)

摘  要:同步轨道卫星在通信、气象、导航定位、对地观测、数据中继等领域应用广泛,对其轨道精度的要求也越来越高。结合国内外卫星系统的高精度测量体制,介绍了我国GEO卫星高精度测定轨技术的2个发展趋势:厘米级高精度多站测距技术和主动CEI测量定轨技术,给出了相应的误差分析、关键技术及解决途径,并介绍了最新试验进展。试验结果表明,给出的2种技术体制均能够实现近10 m量级的GEO卫星实时定轨精度,满足我国GEO卫星的高精度测定轨需求。GEO satellites are widely used in communication,meteorology,navigation and location,earth observation,data relay and other fields.And the requirement of orbit determination precision is also higher and higher.Combining with the high-precision measurement system of satellite system at home and abroad,this paper introduces two development trends of high-precision orbit determination technology for GEO satellites in China:centimeter-level high-precision multi-station ranging technology and CEI measurement and orbit determination technology.The error analysis,key technologies and solutions of the two technologies above are provided,and the recent experimental progress is introduced.The result of the experiment shows that,the two technologies given above can achieve real-time orbit determination accuracy close to 10 meters,which can satisfy the requirements of high-precision orbit determination of GEO satellite in China.

关 键 词:GEO卫星测定轨 高精度伪码测距 连线端干涉测量 高精度时频传递 相位延时测量 

分 类 号:TN871[电子电信—信息与通信工程]

 

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