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e 2 .Motion Earth System Mass Transport Mission (Square) / NGGM-D Team (2014)  

Public Titre : e 2 .Motion Earth System Mass Transport Mission (Square) : Concept for a Next Generation Gravity Field Mission, Final Report of Project “Satellite Gravimetry of the Next Generation (NGGM-D)" Type de document : Rapport Auteurs : NGGM-D Team, Auteur Editeur : Munich : Bayerische Akademie der Wissenschaften Année de publication : 2014 Collection : DGK - B, ISSN 0065-5317 Importance : 200 p. Format : 21 x 30 cm ISBN/ISSN/EAN : 978-3-7696-8597-8 Note générale : Bibliographie Langues : Anglais (eng) Descripteur : [Vedettes matières IGN] Géodésie physique [Termes IGN] champ de pesanteur terrestre [Termes IGN] données GRACE [Termes IGN] masse de la Terre Index. décimale : 30.42 Gravimétrie Résumé : (Auteur) The main goal of this study was the development of a mission concept for the long term high precision and homogeneous determination of the time variable gravity field with significant improved sensitivity and spatial resolution as compared to nowadays techniques, which are used on GRACE and GRACE-FO. This goal is supported by the international science community and is content of resolutions issued by several institutions and science communities like for example resolution No. 2 of the International Union of Geodesy and Geophysics (IUGG; Melbourne, 2011, refer to: http://iugg.org/resolutions). Long duration, higher sensitivity and improved spatial/temporal resolution of mass ariation observations are required by more or less all geoscience disciplines in order to make their models more realistic and in order to assimilate them into these models. Long term analyses and calibration of geophysical models contribute to a better understanding of the coupling of the different phenomena and consequently improve models and provide more realistic prediction capabilities. For this reason, in future a continuous monitoring of mass distribution in the Earth system is required.[...] Note de contenu : 1 NGGM - D Study Approach 2 Sciences and Mission Requirements 3 Orbit Configuration 4 Attitude Determination and Control 5 Instrument Concept 6 Generation of Simulated Observations 7 Numerical Simulations 8 e2 .motion Mission Concept 9 References Annexes Numéro de notice : 15824 Affiliation des auteurs : non IGN Thématique : POSITIONNEMENT Nature : Rapport d'étude technique En ligne : http://dgk.badw.de/fileadmin/docs/b-318.pdf Permalink : https://documentation.ensg.eu/index.php?lvl=notice_display&id=74911

Exemplaires(1)

Code-barres	Cote	Support	Localisation	Section	Disponibilité
15824-01	30.42	Livre	Centre de documentation	Géodésie	Disponible