Acta Geodaetica et Cartographica Sinica ›› 2024, Vol. 53 ›› Issue (12): 2305-2315.doi: 10.11947/j.AGCS.2024.20230176

• Geodesy and Navigation • Previous Articles     Next Articles

Analysis of orbit determination for inclined geosynchronous SAR using spaceborne GNSS data

Peng YANG1,2(), Zhenxing WANG3, Xiaobin TIAN4, Shigui ZHENG5, Yong HUANG1,2,6,7()   

  1. 1.Shanghai Astronomical Observatory, Chinese Academy of Sciences, Shanghai 200030, China
    2.School of Astronomy and Space Science, University of Chinese Academy of Sciences, Beijing 100049, China
    3.Institute of Remote Sensing Satellite, CAST, Beijing 100094, China
    4.Space Star Technology Co., Ltd., Beijing 100000, China
    5.Institute of Spacecraft System Engineering, Beijing 100094, China
    6.Shanghai Key Laboratory of Space Navigation and Positioning Techniques, Shanghai 200030, China
    7.Key Laboratory of Planetary Sciences, Chinese Academy of Sciences, Shanghai 200030, China
  • Received:2023-06-06 Online:2025-01-06 Published:2025-01-06
  • Contact: Yong HUANG E-mail:yangpeng183@mails.ucas.ac.cn;yongh@shao.ac.cn
  • About author:YANG Peng (1996—), male, PhD, majors in spacecraft precision orbit determination and the application. E-mail: yangpeng183@mails.ucas.ac.cn
  • Supported by:
    The Preresearch Project on Civil Aerospace Technologies funded by the China National Space Administration(D010105);The Strategic Priority Research Program of Chinese Academy of Sciences(XDA30040500);The National Key Research and Development Program of China(2020YFC2200903)

Abstract:

With the widespread application of high orbit satellites, the demand for their orbital accuracy is becoming increasingly high. Based on the spaceborne GNSS (global navigation satellite system) data, we simulate an inclined geosynchronous SAR satellite, and analyze the orbit determination accuracy. The results show that the high sensitivity onboard receiver can obtain the signal of about 20 satellites which include GPS and BDS, with PDOP (position dilution of precision) values ranging from 1 to 2. By using the pseudo range/carrier phase measurement values of spaceborne GNSS data, the orbit determination accuracy of inclined geosynchronous SAR satellites can be better than 1 m, and the fluctuation of high-order Legendre error is less than 10 mm. The perturbation of solar radiation pressure has a significant impact on the orbit, the model error of the 10-8 m·s-2 order can reduce the orbit determination accuracy by one order of magnitude.

Key words: high-orbit satellite, spaceborne GNSS, IGSO, SAR satellite, precise orbit determination

CLC Number: