A demonstration of sub meter GPS orbit determination and high precision user positioning

• Published in: IEEE aerospace and electronic systems magazine Vol. 4; no. 2; pp. 16 - 25
• Main Authors: Bertiger, W.I., Lichten, S.M., Katsigris, E.C.
• Format: Magazine Article
• Language: English
• Published: IEEE 01-02-1989
• Subjects: Earth; Global Positioning System; Laboratories; Monitoring; Phase estimation; Propulsion; Satellite broadcasting; Satellite ground stations; Space stations; Space vehicles
• ISSN: 0885-8985; 1557-959X
• DOI: 10.1109/62.16992

High-accuracy orbits have been determined for satellites of the Global Positioning System (GPS), with submeter orbit accuracy demonstrated for two well-tracked satellites. Baselines of up to 2000 km in North America determined with the GPS orbits shows daily repeatability of 0.3-2 parts in 10/sup 8/ and agree with very long baseline interferometry (VLBI) solutions at the level of 1.5 parts in 10/sup 8/. Tests used to assess orbit accuracy include orbit repeatability from independent data sets, orbit prediction, ground baseline determination, and formal errors. One satellite tracked for eight hours each day shows RMS errors below 1 m even when predicted more than three days outside of a 1-week data arc. These results demonstrate the powerful relative positioning capability available from differential GPS tracking. Baselines have also been estimated between Florida and sites in the Caribbean region over 1000 km away, with daily repeatability of 1-4 parts in 10/sup 8/. The best orbit estimation strategies included data arcs of 1-2 weeks, process noise models for tropospheric fluctuations, combined processing of GPS carrier phase and pseudorange data, and estimation of GPS solar pressure coefficients.< >