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Xiaogong Hu

Researcher at Chinese Academy of Sciences

Publications -  6
Citations -  190

Xiaogong Hu is an academic researcher from Chinese Academy of Sciences. The author has contributed to research in topics: Satellite & Orbit determination. The author has an hindex of 5, co-authored 6 publications receiving 155 citations.

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Orbit determination and time synchronization for a GEO/IGSO satellite navigation constellation with regional tracking network

TL;DR: This study estimates orbital elements and clock errors for a 3GEO+2IGSO constellation using a multi-satellite precise orbit determination (MPOD) strategy, with which clock error elimination algorithm is applied to separate orbital and clock estimates to improve numerical efficiency.
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Improvement of orbit determination accuracy for Beidou Navigation Satellite System with Two-way Satellite Time Frequency Transfer

TL;DR: In order to improve the orbit determination accuracy for BDS, a new orbit determination strategy is proposed, in which the satellite clock measurements from TWSTFT are fixed as known values, and only the orbits of the satellites are solved.
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Positioning accuracy assessment for the 4GEO/5IGSO/2MEO constellation of COMPASS

TL;DR: Experiments show that COMPASS PPP repeatability for the east, north and up components of a receiver within mainland China is better than 2 cm, 2 cm and 5 cm, respectively, indicating errors remaining in the treatments of COMPASS measurement and dynamic models and reference frame differences existing between two systems.
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Modeling and initial assessment of the inter-frequency clock bias for COMPASS GEO satellites

TL;DR: In this paper, an apparent inter-frequency clock bias (IFCB) for COMPASS GEO satellites is investigated using the real data, and the bias also is modeled by the different models.
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Orbit determination and prediction for Beidou GEO satellites at the time of the spring/autumn equinox

TL;DR: In this article, a three-step approach of the multi-satellite precise orbit determination (MPOD) was proposed, where pseudo-range (carrier phase) data are transformed to geometric range (biased geometric range) data without clock offsets; and reasonable empirical acceleration parameters are estimated along with orbital elements to account for the error in solar radiation pressure modeling.