Abstract
The precise orbit determination (POD) of low earth orbit (LEO) satellites is always a hotspot topic in the field of satellite geodesy. Current gravity field determination, satellite altimetry, and remote sensing measurement depend crucially on the precise orbits of the spacecraft. BeiDou global navigation satellite system (BDS-3) is officially completed in 2020 and offers positioning, navigation, and timing (PNT) service for global users. The onboard BDS measurements from LEO satellites can be used for LEO POD and served as an effective supplement for BDS tracking geometry. In this study, the BDS-3 observations with B1C and B2a signals of HY-2D spacecraft are employed for reduced-dynamic POD. For superior orbit quality, the extended analytical model for solar radiation pressure (SRP) is used for LEO POD, and in-flight calibration of the LEO receiver antenna is carried out to improve the orbit precision. Two weeks of onboard BDS-3 observation were used to assess the BDS-based POD performance. For HY-2D satellite based on BDS-3 instruments, the capability of continuous tracking is at the global level, and almost all the epochs can have 5–7 usable BDS satellites. The mean root-mean-squared (RMS) of the phase residual obtained from the reduced-dynamic POD is 6.5 mm, and that of pseudorange residual is 1.28 m. The internal precision for the entire arc is in good agreement. Moreover, an orbit self-consistency of 0.94 cm, 0.76 cm, and 0.49 cm is displayed in the along-track, cross-track, and radial directions, respectively.
The 1.33 cm 3D RMS of the internal consistency is achieved for the reduced-dynamic orbits. A better than 2 cm RMS has been achieved in the Satellite Laser Ranging (SLR) validation for BDS-3-based LEO orbit solutions. These results could be used for the Chinese subsequent LEO satellite equipped with a BDS-3 receiver.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Tapley, B.D., Ries, J.C., Davis, G.W., et al.: Precision orbit determination for Topex/Poseidon. J. Geophys. Res. Oceans 99(C12), 24383–24404 (1994)
Flohrer, C., Otten, M., Springer, T., et al.: Generating precise and homogeneous orbits for Jason-1 and Jason-2. Adv. Space Res. 48(1), 152–172 (2011)
Montenbruck, O., Hackel, S., Jäggi, A.: Precise orbit determination of the Sentinel-3A altimetry satellite using ambiguity-fixed GPS carrier phase observations. J. Geodesy 92(7), 711–726 (2018)
Tapley, B.D., Bettadpur, S., Ries, J.C., et al.: GRACE measurements of mass variability in the Earth system. Science 305(5683), 503–505 (2004)
Kang, Z., Tapley, B., Bettadpur, S., et al.: Precise orbit determination for the GRACE mission using only GPS data. J. Geodesy 80(6), 322–331 (2006)
Kornfeld, R.P., Arnold, B.W., Gross, M.A., et al.: GRACE-FO: The Gravity Recovery and Climate Experiment Follow-On Mission [J]. Journal Of Spacecraft And Rockets 56(3), 931–951 (2019)
Bock, H., Jäggi, A., Beutler, G., et al.: GOCE: precise orbit determination for the entire mission. J. Geodesy 88(11), 1047–1060 (2014)
Vielberg, K., Kusche, J.: Extended forward and inverse modeling of radiation pressure accelerations for LEO satellites. J. Geodesy 94(4), 1–21 (2020)
Jing-Nan, L., Mao-Rong, G.: PANDA software and its preliminary result of positioning and orbit determination. Wuhan Univ. J. Nat. Sci. 8(2), 603–609 (2003)
Zhao, Q., Guo, J., Wang, C., et al.: Precise orbit determination for BDS satellites. Satellite Navig. 3(1), 1–24 (2022)
Rebischung, P., Schmid, R.: IGS14/igs14.atx: a new framework for the IGS products; proceedings of the AGU Fall Meeting Abstracts, F (2016)
Schmid, R., Dach, R., Collilieux, X., Jäggi, A., Schmitz, M., Dilssner, F.: Absolute IGS antenna phase center model igs08.atx: status and potential improvements. J. Geodesy 90(4), 343–364 (2015)
Shako, R., Förste, C., Abrikosov, O., Bruinsma, S., Marty, J.-C., Lemoine, J.-M., Flechtner, F., Neumayer, H., Dahle, C.: EIGEN-6C: a high-resolution global gravity combination model including GOCE data. In: Flechtner, F., Sneeuw, N., Schuh, W.-D. (eds.) Observation of the System Earth from Space - CHAMP, GRACE, GOCE and future missions: GEOTECHNOLOGIEN Science Report No. 20, pp. 155–161. Springer Berlin Heidelberg, Berlin, Heidelberg (2014). https://doi.org/10.1007/978-3-642-32135-1_20
Petit, G., Luzum, B.: Bureau International des Poids et mesures sevres (france) (2010)
Lyard, F., Lefevre, F., Letellier, T., et al.: Modelling the global ocean tides: modern insights from FES2004. Ocean Dyn. 56(5), 394–415 (2006)
ILRS: SLRF2014 station coordinates (2020)
Mendes, V.B., Pavlis, E.C.: High-accuracy zenith delay prediction at optical wavelengths. Geophys. Res. Lett. 31(14), 1–5 (2004)
Wang, Y.C., Li, M., Jiang, K.C., et al.: Precise orbit determination of the Haiyang 2C altimetry satellite using attitude modeling. GPS Sol. 26(1), 1–14 (2022)
Wang, Y., et al.: Reduced-dynamic precise orbit determination of Haiyang-2B altimetry satellite using a refined empirical acceleration model. Remote Sensing 13(18), 3702 (2021)
Jäggi, A., Dach, R., Montenbruck, O., et al.: Phase center modeling for LEO GPS receiver antennas and its impact on precise orbit determination. J. Geodesy 83(12), 1145–1162 (2009)
Dow, J.M., Neilan, R.E., Rizos, C.: The international GNSS service in a changing landscape of global navigation satellite systems. J. Geodesy 83(3–4), 191–198 (2009)
Schaer, S., Villiger, A., Arnold, D., Dach, R., Prange, L., Jäggi, A.: The CODE ambiguity-fixed clock and phase bias analysis products: generation, properties, and performance. J. Geodesy 95(7), 1–25 (2021)
Pearlman, M.R., et al.: The ILRS: approaching 20 years and planning for the future. J. Geodesy 93(11), 2161–2180 (2019)
Guo, J.Y., Wang, Y.C., Shen, Y., et al.: Estimation of SLR station coordinates by means of SLR measurements to kinematic orbit of LEO satellites. Earth Planets Space 70(1), 201 (2018)
Drożdżewski, M., Sośnica, K.: Tropospheric and range biases in Satellite Laser Ranging. J. Geodesy 95(9), 1–18 (2021)
Strugarek, D., Sośnica, K., Zajdel, R., Bury, G.: Detector-specific issues in Satellite Laser Ranging to Swarm-A/B/C satellites. Measurement 182, 109786 (2021)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2022 Aerospace Information Research Institute
About this paper
Cite this paper
Wang, Y., Zhao, Q., Jiang, K. (2022). Precise Orbit Determination of LEO Satellite Using Onboard BDS-3 B1C/B2a Observations. In: Yang, C., Xie, J. (eds) China Satellite Navigation Conference (CSNC 2022) Proceedings. Lecture Notes in Electrical Engineering, vol 910. Springer, Singapore. https://doi.org/10.1007/978-981-19-2576-4_12
Download citation
DOI: https://doi.org/10.1007/978-981-19-2576-4_12
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-19-2575-7
Online ISBN: 978-981-19-2576-4
eBook Packages: EngineeringEngineering (R0)