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Satellite Positioning and Orbit Determination System(SPODS):Introduction and Evaluation 被引量:4
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作者 Ziqing WEI Rengui RUAN +5 位作者 Xiaolin JIA xianbing wu Xiaoyong SONG Yue MAO Laiping FENG Yongxing ZHU 《Journal of Geodesy and Geoinformation Science》 2018年第1期25-29,共5页
The Satellite Positioning and Orbit Determination System(SPODS)is a software package for GNSS positioning/orbit determination,developed by the Xi’an Research Institute of Surveying and Mapping.So far it has been able... The Satellite Positioning and Orbit Determination System(SPODS)is a software package for GNSS positioning/orbit determination,developed by the Xi’an Research Institute of Surveying and Mapping.So far it has been able to analyse GPS data and has the capability of high precision GPS positioning and orbit determination.The underlying theory and the performance evaluation are briefly addressed in this paper.The experiments are carried out with GPS data collected from about 127 IGS stations during 4~10 January 2009.The results show that the RMS 1D difference is 1.1 cm between SPODS orbits and final IGS combined orbits,and that the repeatability of daily solutions of station coordinates is 1.5 mm for horizontal components,and 4.5 mm for vertical component,and that the consistency of ERP solutions with IGS final products is 0.025 mas,0.093 mas and 0.013 ms/d respectively for pole coordinates and LOD. 展开更多
关键词 GNSS PRECISE POSITIONING PRECISE ORBIT DETERMINATION ERP DETERMINATION SPODS
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Estimation method of SBAS dual-frequency range error integrity parameter 被引量:2
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作者 Bo Shao Qun Ding xianbing wu 《Satellite Navigation》 2020年第1期93-100,共8页
The development of a dual-frequency multi-constellation satellite-based augmentation system(DFMC SBAS)is in progress worldwide.The broadcasted dual-frequency range error(DFRE)integrity parameter reflects the effects o... The development of a dual-frequency multi-constellation satellite-based augmentation system(DFMC SBAS)is in progress worldwide.The broadcasted dual-frequency range error(DFRE)integrity parameter reflects the effects of satellite ephemeris and clock corrections.A user uses the DFRE to calculate the protection level and then determines whether the DFMC SBAS service satisfies the requirements of the current flight phase.However,the calculation of the DFRE has not been reported.Herein,a DFRE estimation method is proposed based on the projection method.Using the ephemeris-clock covariance matrix of each satellite,the maximal projection direction was solved,and the projection of the covariance matrix on this direction was used as the DFRE to form an envelope for the maximal corrected error.Results show that the DFRE can form an envelope of the maximal corrected error with a set probability,and the integrity performance in the user segment satisfies the Category I precision approach requirement. 展开更多
关键词 Satellite-based augmentation system Dual-frequency multi-constellation Dual-frequency range error INTEGRITY
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