Design and analysis of GPS satellite-based augmentation system based on low earth orbit constellations
Abstract Addressing the need for improved GPS accuracy, especially for low-dynamic users, this study introduces a GPS augmentation system employing Low Earth Orbit (LEO) satellites. We detail the principles of satellite navigation and augmentation and simulate the GPS-LEO constellation to analyse its performance in terms of satellite visibility and Position Dilution of Precision (PDOP). The results demonstrate substantial augmentation in navigation accuracy with the integrated system, as verified by UAV flight experiments. The integration of LEO satellites is anticipated to advance global navigation capabilities, with implications for intelligent transportation, logistics, and precision agriculture.
Authors
- Jianlei Yang (ORCID: https://orcid.org/0000-0001-8424-7040)
- Zhengzhen Jin
- Guoyu Ma (ORCID: https://orcid.org/0000-0002-2853-4747)
- Shuaiyong Zheng (ORCID: https://orcid.org/0000-0003-2286-5059)
- Shengyue Ji (ORCID: https://orcid.org/0000-0002-0393-5149)
- Shiyong Huang (ORCID: https://orcid.org/0009-0009-0855-0449)
Institutions
- Tianjin University of Technology (CN)
- Tianjin Normal University (CN)
- China Electronics Technology Group Corporation (CN)
- Beijing Satellite Navigation Center (CN)
Publication Details
- Journal
- Journal of Physics Conference Series
- Published
- 2025-03-01
- DOI
- https://doi.org/10.1088/1742-6596/2977/1/012025
- Primary Topic
- Inertial Sensor and Navigation
- Type
- article
- Field-Weighted Citation Impact
- 0.00