Descripteur
Termes IGN > 1- Outils - instruments et méthodes > instrument > instrument de navigation > centrale inertielle > centrale inertielle à composants liés
centrale inertielle à composants liés |
Documents disponibles dans cette catégorie (7)
Ajouter le résultat dans votre panier Affiner la recherche Interroger des sources externes
Etendre la recherche sur niveau(x) vers le bas
Impact of temperature stabilization on the strapdown airborne gravimetry: a case study in Central Turkey / Mehmet Simav in Journal of geodesy, vol 94 n°4 (April 2020)
[article]
Titre : Impact of temperature stabilization on the strapdown airborne gravimetry: a case study in Central Turkey Type de document : Article/Communication Auteurs : Mehmet Simav, Auteur ; David Becker, Auteur ; Hasan Yildiz, Auteur ; Matthias Hoss, Auteur Année de publication : 2020 Note générale : bibliographie Langues : Anglais (eng) Descripteur : [Vedettes matières IGN] Géodésie physique
[Termes IGN] accéléromètre
[Termes IGN] centrale inertielle à composants liés
[Termes IGN] contrôle thermique
[Termes IGN] étalonnage d'instrument
[Termes IGN] filtre de Kalman
[Termes IGN] gravimétrie aérienne
[Termes IGN] réalité de terrain
[Termes IGN] température
[Termes IGN] TurquieRésumé : (auteur) Airborne gravimetry with strapdown inertial sensors has been a valuable tool for many years to fill in the gravity data gaps on the areas not accessible by land. Accuracies of 1 mGal level with off-the-shelf navigation-grade inertial measurement units (IMU) can only be achieved provided that the accelerometer drifts mainly caused by the temperature variations inside the IMU housing are separated from the gravity signal. Although there are several strategies proposed in the literature to deal with this inseparability problem, we use a thermal stabilization system (iTempStab) added on an iNAT-RQH navigation-grade IMU and investigate its performance over a test region in central Turkey with moderate topography and highly qualified ground truth gravity data. Two test flights were performed in 2017 and 2018 with and without iTempStab add-on following almost the same flight trajectories. During the first flight in 2017 with iNAT-RQH only, which lasted almost 5.5 h, there were considerable temperature variations inside the IMU housing from 39.1 to 46.0 °C. A simple thermal correction based on a laboratory calibration done before the flight was applied to the vertical Z-accelerometer in the pre-processing stage. However, temperature changes were within 0.1 °C during the second test flight in 2018 with TempStab add-on. The temperature stabilization gained by the iTempStab add-on produced better cross-over statistics. While the RMSE of the non-adjusted cross-over residuals was about 2.6 mGal, it reduced by 50% with iTempStab add-on. The adjusted cross-over differences of the 2018 flight yielded an RMSE of about 0.5 mGal, which is a remarkable precision for the strapdown gravimetry. The comparison with upward continued ground gravity data at flight altitudes suggests that the thermal stabilization system shows also remarkable improvements in the residual statistics. The range of the residuals decreases from ± 10 to ± 5 mGal, the standard deviation decreases from 2.19 to 0.94 mGal, and the RMSE decreases from 2.24 to 1.48 mGal, respectively, with the iTempStab add-on. It can be concluded that the thermal stabilization system significantly improves the accelerometer stability and therefore the precision and accuracy of the strapdown airborne gravity estimates. Numéro de notice : A2020-158 Affiliation des auteurs : non IGN Thématique : POSITIONNEMENT Nature : Article nature-HAL : ArtAvecCL-RevueIntern DOI : 10.1007/s00190-020-01369-5 Date de publication en ligne : 17/03/2020 En ligne : https://doi.org/10.1007/s00190-020-01369-5 Format de la ressource électronique : url article Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=94812
in Journal of geodesy > vol 94 n°4 (April 2020)[article]Development and evaluation of GNSS/INS data processing software for position and orientation systems / X. Niu in Survey review, vol 47 n° 341 (March 2015)
[article]
Titre : Development and evaluation of GNSS/INS data processing software for position and orientation systems Type de document : Article/Communication Auteurs : X. Niu, Auteur ; Qian Zhang, Auteur ; L. Gong, Auteur ; et al., Auteur Année de publication : 2015 Article en page(s) : pp 87 - 98 Note générale : bibliographie Langues : Anglais (eng) Descripteur : [Termes IGN] centrale inertielle à composants liés
[Termes IGN] couplage GNSS-INS
[Termes IGN] filtre de Kalman
[Termes IGN] logiciel de post-traitement GPS
[Termes IGN] traitement de données GNSS
[Vedettes matières IGN] Traitement de données GNSSRésumé : (auteur) Currently there are limited supportive and reliable commercial software packages for GNSS/INS data processing. The shortage of compatible GNSS/INS data processing software has become a bottleneck in the development of position and orientation systems (POS) for survey and mapping applications. Thus this paper introduces a GNSS/INS data processing software called Cinertial, which has been recently developed in China, with open definitions of data format and parameters. The algorithm design of the software is described in detail, including the realisation of INS mechanisation, Kalman filtering, and backward smoothing. The developed software is tested and evaluated by comparing it with mainstream commercial software through processing the same field test datasets. A precise and feasible comparison procedure is proposed in the paper, so as to evaluate the quality of any new POS software in an efficient, convenient, and cost-effective way. The procedure was applied to compare our new software with two well known commercial software packages through processing airborne and terrestrial datasets respectively. The results show that the new software can achieve the same level of accuracy as the current commercial software on the market, which reflects a new progress of the POS development in China. Numéro de notice : A2015-956 Affiliation des auteurs : non IGN Thématique : POSITIONNEMENT Nature : Article DOI : 10.1179/1752270614Y.0000000099 En ligne : http://www.tandfonline.com/doi/full/10.1179/1752270614Y.0000000099 Format de la ressource électronique : URL article Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=79941
in Survey review > vol 47 n° 341 (March 2015) . - pp 87 - 98[article]Hybride Navigationssysteme für Navigation, Regelung und direkte Georeferenzierung / Manfred Bäumker in ZFV, Zeitschrift für Geodäsie, Geoinformation und Landmanagement, vol 138 n° 5 (01/09/2013)
[article]
Titre : Hybride Navigationssysteme für Navigation, Regelung und direkte Georeferenzierung Type de document : Article/Communication Auteurs : Manfred Bäumker, Auteur Année de publication : 2013 Article en page(s) : pp 303 - 312 Note générale : Bibliographie Langues : Allemand (ger) Descripteur : [Vedettes matières IGN] Acquisition d'image(s) et de donnée(s)
[Termes IGN] centrale inertielle
[Termes IGN] centrale inertielle à composants liés
[Termes IGN] drone
[Termes IGN] géoréférencement direct
[Termes IGN] système de numérisation mobileRésumé : (Auteur) Inertial systems have been used for more than WO years for the navigation of vehicles. Due to the unavoidable drift and biases of the inertial sensors (gyros and accelerometers), these systems have to be augmented by additional sensors in accordance with the dead reckoning. With the development of the laser gyro with which the highest accuracy can be achieved, and powerful computers also the development of the strap-down systems started which replaced more and more the former platform systems. Another milestone in the field of navigation was the development of GNSS, which is ideal for coupling with INS systems using the Kalman filter technique. With these hybrid navigation systems, a direct georeferencing of photogrammetric image and scanner data is possible. At the University of Applied Sciences Bochum different systems for aerial flights and for use in land vehicles have been developed in recent years. The latest developments in the field of micro-electro-mechanical systems (MEMS) have been affected in the past the development of inertial sensors and the augmentation sensors as well. Although these sensors do not reach the high accuracies of their predecessors, they are inexpensive and of light weight. The development of these sensors in conjunction with powerful microcontrollers led recently to the rapidly growing use of Unmanned Aerial Vehicles (UAVs) for photogrammetric applications. Especially the so-called Multicopter, which are able to rise vertically and hover over a point are an ideal platform for photogrammetric sensors. In this paper, the various sensors and inertial navigation systems and developments for navigation and control as well as for photogrammetric applications and direct georeferencing, which requires a special calibration method for determining the relative position and orientation of the various sensors, are presented. Numéro de notice : A2013-521 Affiliation des auteurs : non IGN Thématique : IMAGERIE Nature : Article DOI : sans Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=32658
in ZFV, Zeitschrift für Geodäsie, Geoinformation und Landmanagement > vol 138 n° 5 (01/09/2013) . - pp 303 - 312[article]Exemplaires(1)
Code-barres Cote Support Localisation Section Disponibilité 199-2013051 RSREV Revue Centre de documentation Revues en salle Disponible Aufbau eines operablen inertialen Vermessungssystems zur Online-Verarbeitung in der Geodäsie auf Basis eines kommerziellen Strapdown Inertialsystems / O. Heinze (1996)
Titre : Aufbau eines operablen inertialen Vermessungssystems zur Online-Verarbeitung in der Geodäsie auf Basis eines kommerziellen Strapdown Inertialsystems Titre original : [Installation d'une centrale inertielle pour le traitement en ligne en géodésie sur la base d'un système inertiel commercial sans plate-forme] Type de document : Thèse/HDR Auteurs : O. Heinze, Auteur Editeur : Munich : Bayerische Akademie der Wissenschaften Année de publication : 1996 Collection : DGK - C Sous-collection : Dissertationen num. 459 Importance : 67 p. Format : 21 x 30 cm ISBN/ISSN/EAN : 978-3-7696-9502-1 Note générale : Bibliographie Langues : Allemand (ger) Descripteur : [Vedettes matières IGN] Géodésie spatiale
[Termes IGN] centrale inertielle
[Termes IGN] centrale inertielle à composants liés
[Termes IGN] filtre de Kalman
[Termes IGN] GPS-INS
[Termes IGN] traitement du signalIndex. décimale : 30.64 GPS et centrales inertielles Numéro de notice : 28020 Affiliation des auteurs : non IGN Thématique : POSITIONNEMENT Nature : Thèse étrangère Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=63367 Exemplaires(2)
Code-barres Cote Support Localisation Section Disponibilité 28020-01 30.64 Livre Centre de documentation Géodésie Disponible 28020-02 30.64 Livre Centre de documentation Géodésie Disponible Post-Mission Auswertemodell für die Vermessung mit Strapdown Inertialsystemen / S. Röhrich (1993)
Titre : Post-Mission Auswertemodell für die Vermessung mit Strapdown Inertialsystemen Titre original : [Modèle de post-mission pour la mesure avec une centrale inertielle à composants liés] Type de document : Thèse/HDR Auteurs : S. Röhrich, Auteur Editeur : Munich : Bayerische Akademie der Wissenschaften Année de publication : 1993 Collection : DGK - C Sous-collection : Dissertationen num. 407 Importance : 125 p. Format : 21 x 30 cm ISBN/ISSN/EAN : 978-3-7696-9452-9 Note générale : Bibliographie Langues : Allemand (ger) Descripteur : [Vedettes matières IGN] Géodésie spatiale
[Termes IGN] analyse comparative
[Termes IGN] centrale inertielle
[Termes IGN] centrale inertielle à composants liés
[Termes IGN] données localisées 3D
[Termes IGN] filtre de Kalman
[Termes IGN] GPS-INS
[Termes IGN] modèle de Gauss-Markov
[Termes IGN] précision des mesures
[Termes IGN] précision du positionnementIndex. décimale : 30.64 GPS et centrales inertielles Résumé : (Auteur) This work presents a postmission-model for data-evaluation of strapdown inertial navigation systems (INS) which is also modified for classical platform systems. The main aspect of this model is to increase the accuracy of strapdown systems to use them for geodetic applications.
The determination of state parameters, which describe the physical behaviour of the navigation errors is the main point. The mathematical equations in this model are derived from the Kalman-filter-algorithm. Instead of this algorithm which is used for on line processing, the state parameters are estimated off line in a Gauss-Markov-model, in use of all measurement data. Using mechanical equations of a horizontal orientated navigation system, an physical interpreta-tion of the state parameters is given.
The test measurements, under geodetic conditions has been carried out with the LASERNAV II from HONEYWELL, a strapdown navigationsystem, and in one case with the ULISS 30 from SAGEM, a conventional platform system. The influence of the configuration of the measurement on the accuracy is tested in the case of the LASERNAV II.
The results of the LASERNAV II and ULISS 30 are compared. The achieved accura-cies in position are about some dm for strapdown systems and cm for platform systems.
Furthermore measurements with INS/GPS combination complete the numerical tests and present an application of this model for measurements in aircrafts. With the achieved results, it is shown that strapdown INS can be used for some geodetic applications. Further theoretical aspects to integrate the inertial gravimetry in this model are described.Numéro de notice : 28076 Affiliation des auteurs : non IGN Thématique : POSITIONNEMENT Nature : Thèse étrangère Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=63423 Exemplaires(2)
Code-barres Cote Support Localisation Section Disponibilité 28076-01 30.64 Livre Centre de documentation Géodésie Disponible 28076-02 30.64 Livre Centre de documentation Géodésie Disponible Systèmes inertiels à composants liés - strap-down / Jean-Claude Radix (1993)PermalinkAufbau eines geodätischen Strapdown Inertialsystems zur Punktbestimmung / D. Keller (1991)Permalink