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Generating statistically robust multipath stacking maps using congruent cells / Thomas Fuhrmann in GPS solutions, vol 19 n° 1 (January 2015)
[article]
Titre : Generating statistically robust multipath stacking maps using congruent cells Type de document : Article/Communication Auteurs : Thomas Fuhrmann, Auteur ; Xiaoguang Luo, Auteur ; Andreas Knöpfler, Auteur ; Michael Mayer, Auteur Année de publication : 2015 Article en page(s) : pp 83 - 92 Note générale : bibliographie Langues : Anglais (eng) Descripteur : [Vedettes matières IGN] Géodésie spatiale
[Termes IGN] congruence
[Termes IGN] correction du trajet multiple
[Termes IGN] résidu
[Termes IGN] superposition
[Termes IGN] trajet multiple
[Termes IGN] valeur aberranteRésumé : (auteur) Multipath effects caused by reflections in the near-field and far-field of a GNSS antenna represent a major error source in static and kinematic GNSS positioning applications. Since these effects are strongly site-specific, a generally valid and practicable analytical multipath model is still lacking. In contrast, using GNSS carrier phase observation residuals, the multipath stacking (MPS) methods are able to take site-specific conditions into account. We propose an advanced approach to performing residual-based MPS in the space domain. Being superior to most conventional attempts in which stacking cells have a fixed azimuthal resolution, our suggested method makes use of congruent cells and rigorous statistical assessments in terms of outlier detection and significance evaluation of the stacked values. The advanced stacking approach is applied to representative phase residuals from static precise point positioning. The results show that the use of congruent cells allows for MPS at high elevation angles and with a fine spatial resolution. Applying the resulting MPS maps at the residual level, both near-field and far-field effects at high and low elevation angles, respectively, can be significantly mitigated. In comparison with the conventional approach, the advanced one enables a larger reduction of about 20 % in the SD of residuals. Numéro de notice : A2015-205 Affiliation des auteurs : non IGN Thématique : POSITIONNEMENT Nature : Article DOI : 10.1007/s10291-014-0367-7 Date de publication en ligne : 23/02/2014 En ligne : https://doi.org/10.1007/s10291-014-0367-7 Format de la ressource électronique : URL article Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=76018
in GPS solutions > vol 19 n° 1 (January 2015) . - pp 83 - 92[article]The carrier-multipath observable: a new carrier-phase multipath mitigation technique / Ramin Moradi in GPS solutions, vol 19 n° 1 (January 2015)
[article]
Titre : The carrier-multipath observable: a new carrier-phase multipath mitigation technique Type de document : Article/Communication Auteurs : Ramin Moradi, Auteur ; Wolfgang Schuster, Auteur ; Shaojun Feng, Auteur ; et al., Auteur Année de publication : 2015 Article en page(s) : pp 73 - 82 Note générale : bibliographie Langues : Anglais (eng) Descripteur : [Vedettes matières IGN] Géodésie spatiale
[Termes IGN] correction du trajet multiple
[Termes IGN] trajet multipleRésumé : (auteur) Modeling and mitigating carrier-phase multipath errors continue to be a significant challenge for high-accuracy positioning using global navigation satellite systems. The multipath error is dependent on the operational environment and therefore cannot be mitigated by differencing techniques. The effect of multipath is accentuated when observables based on linear combinations of measurements from two or more frequencies are formulated. We develop a new carrier-phase multipath error observable that isolates the inter-frequency carrier-phase multipath error for linear combinations of observables, such as wide-lane (WL). Real-time kinematic positioning results from varying baseline lengths show that a significant reduction in between 14 and 47 % in the time to initial ambiguity resolution are achieved by correcting the WL observable using the new carrier-phase multipath error observable. Numéro de notice : A2015-204 Affiliation des auteurs : non IGN Thématique : POSITIONNEMENT Nature : Article DOI : 10.1007/s10291-014-0366-8 Date de publication en ligne : 22/01/2014 En ligne : https://doi.org/10.1007/s10291-014-0366-8 Format de la ressource électronique : URL article Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=76017
in GPS solutions > vol 19 n° 1 (January 2015) . - pp 73 - 82[article]Accounting for Galileo–GPS inter-system biases in precise satellite positioning / Jacek Paziewski in Journal of geodesy, vol 89 n° 1 (January 2015)
[article]
Titre : Accounting for Galileo–GPS inter-system biases in precise satellite positioning Type de document : Article/Communication Auteurs : Jacek Paziewski, Auteur ; Pawel Wielgosz, Auteur Année de publication : 2015 Article en page(s) : pp 81 - 93 Note générale : Bibliographie Langues : Anglais (eng) Descripteur : [Vedettes matières IGN] Géodésie spatiale
[Termes IGN] acquisition de données
[Termes IGN] analyse comparative
[Termes IGN] données GNSS
[Termes IGN] double différence
[Termes IGN] erreur systématique
[Termes IGN] fusion de données
[Termes IGN] positionnement différentiel
[Termes IGN] signal Galileo
[Termes IGN] signal GPS
[Termes IGN] stabilité dans le tempsRésumé : (auteur) Availability of two overlapping frequencies L1/E1 and L5/E5a of the signals transmitted by GPS and Galileo systems offers the possibility of tightly combining observations from both systems in a single observational model. A tightly combined observational model assumes a single reference satellite for all observations from both Galileo and GPS systems. However, when inter-system double-differenced observations are created, receiver inter-system bias is introduced. This study presents the results and the methodology for estimation and accounting for phase and code GPS-Galileo inter-system bias in precise relative positioning. The research investigates the size and temporal stability of the estimated bias for different receiver pairs as well as examines the influence of accounting for the inter-system bias on the user position solution. The obtained numerical results are based on four experiments carried out at different locations and time periods using both real and simulated GNSS data. Numéro de notice : A2015-329 Affiliation des auteurs : non IGN Thématique : POSITIONNEMENT Nature : Article nature-HAL : ArtAvecCL-RevueIntern DOI : 10.1007/s00190-014-0763-3 En ligne : https://doi.org/10.1007/s00190-014-0763-3 Format de la ressource électronique : URL article Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=76654
in Journal of geodesy > vol 89 n° 1 (January 2015) . - pp 81 - 93[article]Determination of precise satellite orbits and geodetic parameters using satellite laser ranging / Krzysztof Sosnica (2015)
Titre : Determination of precise satellite orbits and geodetic parameters using satellite laser ranging Type de document : Rapport Auteurs : Krzysztof Sosnica, Auteur Editeur : Zurich : Schweizerischen Geodatischen Kommission / Commission Géodésique Suisse Année de publication : 2015 Collection : Geodätisch-Geophysikalische Arbeiten in der Schweiz, ISSN 0257-1722 num. 93 Importance : 257 p. Format : 21 x 30 cm ISBN/ISSN/EAN : 978-3-908440-38-3 Note générale : bibliographie Langues : Anglais (eng) Descripteur : [Vedettes matières IGN] Géodésie spatiale
[Termes IGN] Bernese
[Termes IGN] données Ajisai
[Termes IGN] données Lageos
[Termes IGN] données Starlette
[Termes IGN] données Stella
[Termes IGN] géocentre
[Termes IGN] Global Geodetic Observing System
[Termes IGN] orbite basse
[Termes IGN] perturbation orbitale
[Termes IGN] repère de référence
[Termes IGN] rotation de la Terre
[Termes IGN] satellite de télémétrie
[Termes IGN] télémétrie laser sur satelliteIndex. décimale : 30.63 Télémétrie laser sur satellite, Télémétrie laser sur lune, VLBI Résumé : (auteur) The contribution of the SLR to the definition of the origin of reference frame (geocenter coordinates), the global scale (in both the geometric and dynamic sense), and low degree coefficients of the Earth's gravity field (especially the oblateness term) is essential, due to the high stability of satellite orbits and the exceptional precision of SLR observations, which are affected only by few error sources. Moreover, the SLR technique has a great contribution to a definition of the global terrestrial reference frame, estimation of the Earth rotation parameters and the time variable Earth's gravity field. The long time series of precise SLR observations allow validating many models, e.g., ocean tide models, Earth gravity field models, atmospheric pressure loading models, atmosphere and ocean induced time variable gravity field models, etc. We have shown that appropriate modeling of gravitational and non-gravitational forces is essential for orbit determination of geodetic satellites. Concerning the gravitational forces, the coefficient C20 couses the largest perturbations on LAGEOS satellites. The sensitivity of LAGEOS orbits dramatically decreases for higher degree geopotential coefficients, whereas low orbiting geodetic satellites are very sensitive to both, low- and medium-degree coefficients of the Earth's gravity field. The differences between the current ocean tide models have bigger impact on LAGEOS orbits than the differences between the current Earth gravity field models. The mean differences between solutions using various ocean tide models (max. 1.32 mm of RMS) are larger than the mean differences between orbit solutions using various Earth gravity field models (max. 1.16 mm of RMS). Insufficient quality of the S2 tide constituent causes large variations of the empirical orbit parameters of SLR geodetic satellites, as well as variations for different type satellites, e.g., GRACE. The atmospheric drag causes a secular decay of semi-major axes of low orbiting geodetic satellites, i.e., Starlette, Stella, and AJISAI, whereas the Yarkovsky and the Yarkovsky- Schach effects cause a secular decay of LAGEOS-1 and LAGEOS-2. The decay of the semi-major axis of LAGEOS-1 is smaller than the decay reported in many earlier papers due to the satellite's de-spinning effect. The decay is fiaL1 = Note de contenu : 1 Introduction
1.1 Role of Satellite Laser Ranging in Science
1.2 Objectives and Methods
1.3 Structure
2 Satellite Geodesy
2.1 Reference Systems and Frames
2.2 Satellite Orbit Modeling
2.3 Parameter Estimation Using the Least-Squares Method
2.4 Global Navigation Satellite Systems (GNSS)
2.5 Satellite Laser Ranging
3 Gravitational Forces Acting on Geodetic Satellites
3.1 Solution Description
3.2 LAGEOS Sensitivity to Earth Gravity Field Models
3.3 LAGEOS Sensitivity to Ocean Tide Models
3.4 Discussion and Conclusions
4 Non-gravitational Forces Acting on Geodetic Satellites
4.1 Thermal effects
4.2 Earth Radiation Pressure
4.3 Atmospheric Drag
4.4 Discussion and Conclusions
5 Improving SLR Solutions
5.1 Impact of Loading Corrections on SLR Solutions
5.2 The Blue-Sky effect
5.3 Orbit Modeling of Low Orbiting Geodetic Satellites
5.4 Combined LAGEOS-LEO Solutions
5.5 Simultaneous Estimation of Gravity Field along with other Parameters
5.6 Time Variable Earth's Gravity Field From SLR
5.7 Discussion and ConclusionsNuméro de notice : 14914 Affiliation des auteurs : non IGN Thématique : POSITIONNEMENT Nature : Rapport de recherche DOI : sans En ligne : https://www.sgc.ethz.ch/sgc-volumes/sgk-93.pdf Format de la ressource électronique : URL Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=76821 Exemplaires(1)
Code-barres Cote Support Localisation Section Disponibilité 14914-01 30.63 Livre Centre de documentation Géodésie Disponible First Galileo FOC satellite on the air: Will be employable for surveying, precise positionning, and geodesy / Peter Steingenberger in GPS world, vol 26 n° 1 (January 2015)
[article]
Titre : First Galileo FOC satellite on the air: Will be employable for surveying, precise positionning, and geodesy Type de document : Article/Communication Auteurs : Peter Steingenberger, Auteur ; André Hauschild, Auteur Année de publication : 2015 Article en page(s) : pp 8 -13 Langues : Anglais (eng) Descripteur : [Vedettes matières IGN] Géodésie spatiale
[Termes IGN] positionnement par Galileo
[Termes IGN] positionnement par GNSS
[Termes IGN] signal GalileoIndex. décimale : 30.61 Systèmes de Positionnement par Satellites du GNSS Résumé : (Auteur ) [introduction] The first Full Operational Capability (FOC) Galileo satellite started transmitting L-band navigation signals on november 29, 2014. Numéro de notice : A2015-002 Affiliation des auteurs : non IGN Thématique : POSITIONNEMENT Nature : Article DOI : sans En ligne : http://gpsworld.com/first-galileo-foc-satellite-on-the-air/ Format de la ressource électronique : URL Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=74883
in GPS world > vol 26 n° 1 (January 2015) . - pp 8 -13[article]Exemplaires(1)
Code-barres Cote Support Localisation Section Disponibilité 067-2015011 RAB Revue Centre de documentation En réserve L003 Disponible Global geodetic observatories / Claude Boucher in Advances in space research, vol 55 n° 1 ([01/01/2015])PermalinkPermalinkGPS for land surveyors / Jan Van Sickle (2015)PermalinkGPS satellite surveying / Alfred Leick (2015)PermalinkPermalinkPermalinkPermalinkPermalinkPermalinkPermalink