Phase residuals analysis in kinematic orbit determination of GRACE-FO

被引:0
|
作者
Zhang, Rui [1 ]
Xiong, Yongliang [1 ]
Xu, Shaoguang [1 ]
机构
[1] Southwest Jiaotong Univ, Fac Geosci & Engn, Chengdu, Sichuan, Peoples R China
关键词
Phase residuals; Kinematic orbit determination; Multipath; PCV; Zero-difference; HIGH-FREQUENCY MULTIPATH; GPS RECEIVER ANTENNA; WAVELET TRANSFORM; SATELLITE; MITIGATION; IMPACT; VALIDATION; JASON-1; ERROR;
D O I
10.1016/j.asr.2024.11.008
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The GRACE-FO based scientific research will benefit from the improvement of the kinematic orbit quality. This study investigated the errors that could potentially impact the accuracy of orbit determination and applied error corrections to the observations, including phase center variation (PCV) and multipath error, with a specific focus on enhancing the performance of GRACE-FO kinematic precise orbit determination based on the zero-difference method. When the observation model for precise orbit determination is highly consistent with the actual situation, the phase residuals should only consist of observation noise. However, the phase residuals encompass both modeled errors and unmodeled errors, such as PCV and multipath errors. The study utilized the GPS observation data of the GRACE-FO satellites in January 2022 to derive the fixed ambiguity solutions based on the zero-difference ionosphere-free linear combination, thereby obtaining the phase residuals. Subsequently, the antenna PCV was estimated based on the residual method, resulting in a substantial reduction in carrier phase residuals through PCV correction. A comparison with the reference orbits revealed that the root mean square (RMS) of the fixed solutions with PCV correction improved by 2.8 to 4.3 mm in three directions. Furthermore, the wavelet decomposition was performed on the phase residuals to extract the multipath errors and reconstruct the carrier phase observations. The RMS of the kinematic orbits improved by 4.3 to 5.9 mm with the incorporation of both the PCV and multipath error corrections. The RMS of the satellite laser ranging (SLR) residuals of the two GRACE-FO (GRACE-C and GRACE-D) satellites were 1.43 cm and 1.48 cm, respectively. The results indicate that these methods have the potential to enhance the kinematic orbit accuracy of the GRACE-FO satellites, bringing it closer to the a posteriori scientific orbit accuracy. (c) 2024 COSPAR. Published by Elsevier B.V. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/).
引用
收藏
页码:2048 / 2061
页数:14
相关论文
共 50 条
  • [1] Relative Kinematic Orbit Determination for GRACE-FO Satellite by Jointing GPS and LRI
    Yang, Zhouming
    Liu, Xin
    Guo, Jinyun
    Guo, Hengyang
    Li, Guowei
    Kong, Qiaoli
    Chang, Xiaotao
    REMOTE SENSING, 2022, 14 (04)
  • [2] GRACE-FO precise orbit determination and gravity recovery
    Z. Kang
    S. Bettadpur
    P. Nagel
    H. Save
    S. Poole
    N. Pie
    Journal of Geodesy, 2020, 94
  • [3] GRACE-FO precise orbit determination and gravity recovery
    Kang, Z.
    Bettadpur, S.
    Nagel, P.
    Save, H.
    Poole, S.
    Pie, N.
    JOURNAL OF GEODESY, 2020, 94 (09)
  • [4] Undifferenced Kinematic Precise Orbit Determination of Swarm and GRACE-FO Satellites from GNSS Observations
    Luo, Peng
    Jin, Shuanggen
    Shi, Qiqi
    SENSORS, 2022, 22 (03)
  • [5] A strategy to determine GRACE-FO kinematic orbit during the activation of flex power
    Meng, Guanlong
    Ge, Haibo
    Wu, Tianhao
    Li, Bofeng
    GPS SOLUTIONS, 2025, 29 (02)
  • [6] Improved GRACE-FO kinematic orbit determination with epoch-difference KBR during the GPS flex power period
    Zhang, Jiahui
    You, Wei
    Yu, Biao
    Fan, Dongming
    ADVANCES IN SPACE RESEARCH, 2024, 74 (05) : 2011 - 2024
  • [7] Refinement of GRACE-FO Kinematic Orbit by Combining Least Squares Method and Orbital Dynamic Model
    Ma, Yi
    Yang, Zhouming
    Yuan, Yunbin
    Sun, Qinglei
    Zhou, Fangrong
    Wen, Gang
    JOURNAL OF SENSORS, 2023, 2023
  • [8] On GPS data quality of GRACE-FO and GRACE satellites: effects of phase center variation and satellite attitude on precise orbit determination
    Yaowei Xia
    Xin Liu
    Jinyun Guo
    Zhouming Yang
    Linhu Qi
    Bing Ji
    Xiaotao Chang
    Acta Geodaetica et Geophysica, 2021, 56 : 93 - 111
  • [9] On GPS data quality of GRACE-FO and GRACE satellites: effects of phase center variation and satellite attitude on precise orbit determination
    Xia, Yaowei
    Liu, Xin
    Guo, Jinyun
    Yang, Zhouming
    Qi, Linhu
    Ji, Bing
    Chang, Xiaotao
    ACTA GEODAETICA ET GEOPHYSICA, 2021, 56 (01) : 93 - 111
  • [10] Article GRACE-FO Antenna Phase Center Modeling and Precise Orbit Determination with Single Receiver Ambiguity Resolution
    Jin, Biao
    Li, Yuqiang
    Jiang, Kecai
    Li, Zhulian
    Chen, Shanshan
    REMOTE SENSING, 2021, 13 (21)