If you wish to contribute or participate in the discussions about articles you are invited to contact the Editor
GNSS Satellites Orbit: Difference between revisions
Jump to navigation
Jump to search
Carlos.Lopez (talk | contribs) No edit summary |
Carlos.Lopez (talk | contribs) No edit summary |
||
| Line 3: | Line 3: | ||
|Title={{PAGENAME}} | |Title={{PAGENAME}} | ||
|Authors= J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain. | |Authors= J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain. | ||
|Level= | |Level=Basic | ||
|YearOfPublication=2011 | |YearOfPublication=2011 | ||
|Logo=gAGE | |Logo=gAGE | ||
Revision as of 15:37, 27 October 2011
| Fundamentals | |
|---|---|
| Title | GNSS Satellites Orbit |
| Author(s) | J. Sanz Subirana, JM. Juan Zornoza and M. Hernandez-Pajares, University of Catalunia, Spain. |
| Level | Basic |
| Year of Publication | 2011 |
The knowledge of the orbits and clocks of the satellites is fundamental to have a right positioning. Any error in the GNSS} satellite coordinates or satellite clock will affect the positioning accuracy. Information about orbital parameters and clocks is transmitted in the navigation message. Precise ephemeris and clocks are also provided by some organisations as IGS.
In the following articles, orbital elements are defined, the navigation message is introduced, and the algorithms for satellite coordinate calculation from the GNSS (GPS,GLONASS and Galileo) broadcast and precise ephemeris are detailed.