GNSS ambiguity resolution with optimally controlled failure-rate
| dc.contributor.author | Teunissen, Peter | |
| dc.date.accessioned | 2017-01-30T11:06:32Z | |
| dc.date.available | 2017-01-30T11:06:32Z | |
| dc.date.created | 2012-06-11T02:32:57Z | |
| dc.date.issued | 2005 | |
| dc.identifier.citation | Teunissen, P.J.G. 2005. GNSS ambiguity resolution with optimally controlled failure-rate. Artificial Satellites. 40 (4): pp. 219-227. | |
| dc.identifier.uri | http://hdl.handle.net/20.500.11937/8424 | |
| dc.description.abstract |
GNSS carrier phase ambiguity resolution is the key to fast and high- precision satellite positioning and navigation. It applies to a great variety of current and future models of GPS, modernized GPS and Galileo. In [Teunissen, 2003] we described the general principle of integer aperture (IA) ambiguity estimation. In the present contribution we will derive the optimal IA-estimator. The optimal IA-estimator is defined as the estimator which has the largest possible success rate given a user-defined fail rate. Hence, it is the optimal estimator for which the fail rate can be controlled. | |
| dc.publisher | Versita | |
| dc.subject | Optimal Aperture Estimation | |
| dc.subject | GNSS Ambiguity Resolution | |
| dc.subject | Integer Least-Squares | |
| dc.title | GNSS ambiguity resolution with optimally controlled failure-rate | |
| dc.type | Journal Article | |
| dcterms.source.volume | 40 | |
| dcterms.source.number | 4 | |
| dcterms.source.startPage | 219 | |
| dcterms.source.endPage | 227 | |
| dcterms.source.issn | 0208841X | |
| dcterms.source.title | Artificial Satellites | |
| curtin.department | Delft University of Technology | |
| curtin.accessStatus | Open access |