Aug 2026· Satellite Navigation· Vol 7· 0 citations· 42 references
Abstract
Low Earth Orbit (LEO) navigation augmentation is widely recognized as a key development for next-generation Global Navigation Satellite System (GNSS), and its performance must be validated using real observations. This paper investigates the contribution of LEO satellites to the enhancement of both BeiDou-3 Navigation Satellite System (BDS-3) Precise Orbit Determination (POD) and Precise Point Positioning (PPP) using real observations collected from multiple CENTISPACE™ satellites, which are equipped with both onboard GNSS receivers and navigation augmentation signal transmitters. First, the BDS-3/LEO integrated POD is conducted using BDS-3/CENTISPACE™ downlink observations collected from regional ground stations together with onboard BDS-3 observations from the LEO satellites. Based on these observations, BDS-3 precise orbits and clock offsets, LEO precise orbits and onboard receiver clock offsets, as well as LEO transmitter clock offsets are estimated and evaluated. The results show that incorporating 1–5 LEO satellites significantly enhances the performance of BDS-3 POD. Specifically, the Three-Dimension (3D) orbit accuracy of Medium Earth Orbit (MEO) satellites improves from 54.7 cm using regional ground stations alone to 11.4 cm after integrating five LEO satellites, representing a 79% improvement. In integrated POD, the CENTISPACE™ LEO satellite orbits achieve an accuracy better than 5 cm, and the averaged standard deviation of the clock errors is 0.22 ns. The generated satellite orbits and transmitter clock offsets of both BDS-3 and CENTISPACE™ satellites are subsequently used for BDS-3/LEO PPP. The positioning results from 12 stations show that the convergence time of the BDS-3 kinematic PPP float solution is reduced from 22.4 to 10.8 min when two LEO satellites are integrated, corresponding to a reduction of 51.8%. These results confirm the dual role of LEO satellites in improving BDS-3 POD and PPP performance.
A fundamental limitation of Autonomous Orbit Determination (AOD) for Global Navigation Satellite Systems (GNSS) constellations using Inter-Satellite Links (ISLs) is the inherent unobservability of the overall rotational bias, leading to continuous degradation of orbit determination accuracy. To address this limitation,...
This study proposes a two-step distributed autonomous orbit determination (AOD) and broadcast ephemeris generation framework and demonstrates that the proposed method reduces the broadcast ephemeris user range error (URE) by more than 19% for GRACE-FO satellites and by 44.4% for a multi-satellite LEO constellation comp...
Shuang Sun, Hong-Zhou Chai, Min Wang et al.· GPS Solutions· 0 citations
Onboard global navigation satellite system (GNSS) receivers have become the most convenient means to realize autonomous orbit determination and clock estimation for low Earth orbit (LEO) satellites. However, signal outages and blockages in complex space environments cause GNSS observation degradation, which restricts t...
Xi Chen, Hang Gong, Zong-Nan Li et al.· Measurement science and tech...· 0 citations
The objective of this paper is to demonstrate the future impact of a dedicated low-earth-orbit (LEO) Global Navigation Satellite System (GNSS) on positioning, navigation, and timing (PNT), in addition to a reflective discussion on how common GNSS evaluation methods can best reflect LEO satellite dynamics. This paper wi...
Claire Mah, T. Marathe, Ananya Vishwanath et al.· ION GNSS+, The International...· 0 citations
The use of signals from Earth-orbiting Global Navigation Satellite System (GNSS) constellations for positioning, navigation, and timing on the lunar surface was recently demonstrated by the Lunar GNSS Receiver Experiment (LuGRE) aboard Blue Ghost Mission 1. For receiver clock synchronization using GNSS, Kalman filter p...
Min-Ju Han, Seunghyeon Park, Joon Hyo Rhee· 0 citations
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