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Research on Clock Correction Positioning Method Based on Low Earth Orbit Single Satellite
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Jia SU1, Xiaohui JIN1, Qingwu YI2, 3, *, Hongchi SUN3
Journal of Geodesy and Geodynamics | 2025, 45(5) : 482 - 487
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Journal of Geodesy and Geodynamics | 2025, 45(5): 482-487
Research on Clock Correction Positioning Method Based on Low Earth Orbit Single Satellite
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Jia SU1, Xiaohui JIN1, Qingwu YI2, 3, *, Hongchi SUN3
Affiliations
  • 1 School of Information Science and Engineering, Hebei University of Science and Technology, 26 Yuxiang Street, Shijiazhuang 050018, China
  • 2 National Key Laboratory of Radar Single Processing, Xidian University, 2 South-Taibai Road, Xi'an 710071, China
  • 3 State Key Laboratory of Satellite Navigation System and Equipment Technology, 589 West-Zhongshan Road, Shijiazhuang 050081, China
  • SU Jia, PhD, professor, majorsin wireless communication technology andtarget detection andtracking, E-mail:

About Author:

SU Jia, PhD, professor, majorsin wireless communication technology andtarget detection andtracking, E-mail:

Published: 2025-05-15 doi: 10.14075/j.jgg.2024.06.278
Outline
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Aiming at the problems of poor positioning accuracy, slow convergence speed, and large influence of clock drift in the case of single-satellite positioning methods, a joint pseudo-ranging/Doppler positioning model with clock-difference correction is proposed, which combines the mathematical model of clock-difference with the pseudo-ranging observation equations and Doppler observation equations, and eliminates the influence of the change of the receiver's clock-difference on the positioning accuracy through the simultaneous estimation of clock drift by the mathematical model of clock-difference and the Doppler observation equations. The proposed method is validated in a simulation scenario, and the results show that the optimal positioning accuracy of the pseudorange/Doppler joint positioning with clock difference correction can reach 219 m under different working conditions, which is 59.4% higher than that of the Doppler localization method; when the pseudorange measurement error is 1 m, the positioning accuracy can be up to 169 m, and the convergence time is around 300 s; when the frequency measurement error is 0.5 Hz, the positioning accuracy can be around 140 m.

low earth orbit satellite  /  clock bias correction  /  pseudorange  /  Doppler
苏佳, 靳晓会, 易卿武, 孙洪驰. 基于低轨单星的钟差修正定位方法. 大地测量与地球动力学, 2025 , 45 (5) : 482 -487 . DOI: 10.14075/j.jgg.2024.06.278
Jia SU, Xiaohui JIN, Qingwu YI, Hongchi SUN. Research on Clock Correction Positioning Method Based on Low Earth Orbit Single Satellite[J]. Journal of Geodesy and Geodynamics, 2025 , 45 (5) : 482 -487 . DOI: 10.14075/j.jgg.2024.06.278
  • National Key Research and Development Program of China(2021YFF0603903)
Year 2025 volume 45 Issue 5
39
15
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Article Info
doi: 10.14075/j.jgg.2024.06.278
  • Receive Date:2024-06-12
  • Online Date:2026-10-30
  • Published:2025-05-15
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History
  • Received:2024-06-12
Funding
National Key Research and Development Program of China(2021YFF0603903)
Affiliations
    1 School of Information Science and Engineering, Hebei University of Science and Technology, 26 Yuxiang Street, Shijiazhuang 050018, China
    2 National Key Laboratory of Radar Single Processing, Xidian University, 2 South-Taibai Road, Xi'an 710071, China
    3 State Key Laboratory of Satellite Navigation System and Equipment Technology, 589 West-Zhongshan Road, Shijiazhuang 050081, China
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表12种不同金属材料的力学参数
科
Family
属数
Number of
genus
种数
Number of
species
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Percentage of
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Genus
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Number of
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Percentage of total
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鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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