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Initial Assessment of the LEO Based Navigation Signal Augmentation System from Luojia-1A Satellite

1
State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing, Wuhan University, Wuhan 430079, China
2
Collaborative Innovation Center for Geospatial Technology, Wuhan, 430079, China
3
State Key Laboratory of Satellite Navigation System and Equipment Technology, Shijiazhuang 050000, China
*
Author to whom correspondence should be addressed.
Sensors 2018, 18(11), 3919; https://doi.org/10.3390/s18113919
Received: 29 September 2018 / Revised: 6 November 2018 / Accepted: 12 November 2018 / Published: 14 November 2018
(This article belongs to the Special Issue The Design, Data Processing and Applications of Luojia 1-01 Satellite)
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Abstract

A low Earth orbiter (LEO)-based navigation signal augmentation system is considered as a complementary of current global navigation satellite systems (GNSS), which can accelerate precise positioning convergence, strengthen the signal power, and improve signal quality. Wuhan University is dedicated to LEO-based navigation signal augmentation research and launched one scientific experimental satellite named Luojia-1A. The satellite is capable of broadcasting dual-frequency band ranging signals over China. The initial performance of the Luojia-1A satellite navigation augmentation system is assessed in this study. The ground tests indicate that the phase noise of the oscillator is sufficiently low to support the intended applications. The field ranging tests achieve 2.6 m and 0.013 m ranging precision for the pseudorange and carrier phase measurements, respectively. The in-orbit test shows that the internal precision of the ephemeris is approximate 0.1 m and the clock stability is 3 × 10−10. The pseudorange and carrier phase measurement noise evaluated from the geometry-free combination is about 3.3 m and 1.8 cm. Overall, the Luojia-1A navigation augmentation system is capable of providing useable LEO navigation augmentation signals with the empirical user equivalent ranging error (UERE) no worse than 3.6 m, which can be integrated with existing GNSS to improve the real-time navigation performance. View Full-Text
Keywords: Luojia-1A satellite; satellite-based augmentation system; GNSS signal augmentation; LEO navigation Luojia-1A satellite; satellite-based augmentation system; GNSS signal augmentation; LEO navigation
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Wang, L.; Chen, R.; Li, D.; Zhang, G.; Shen, X.; Yu, B.; Wu, C.; Xie, S.; Zhang, P.; Li, M.; Pan, Y. Initial Assessment of the LEO Based Navigation Signal Augmentation System from Luojia-1A Satellite. Sensors 2018, 18, 3919.

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