Next generation gravity mission: status of the design and discussion on alternative drag compensation scenarios

2020 ◽  
Author(s):  
Luca Massotti ◽  
Gino Bruno Amata ◽  
Alberto Anselmi ◽  
Stefano Cesare ◽  
Philippe Martimort ◽  
...  
Keyword(s):  
Next Generation ◽  
Gravity Mission

Future Gravity Mission Concepts for Sustained Observation of Mass Transport in the Earth System

2021 ◽  
Author(s):  
Roland Pail
Keyword(s):  
Mass Transport ◽  
Closed Loop ◽  
Cold Atom ◽  
Radial Component ◽  
Transport Processes ◽  
Single Pair ◽  
Earth System ◽  
Next Generation ◽  
The Earth ◽  
Gravity Mission

<p>Next Generation Gravity Missions are expected to enhance our knowledge of mass transport processes in the Earth system, establishing their products applicable to new scientific fields and serving societal needs. Compared to the current situation (GRACE Follow-On), a significant step forward to increase spatial and temporal resolution can only be achieved by new mission concepts, complemented by improved instrumentation and tailored processing strategies.</p><p>In extensive numerical closed-loop mission simulations studies, different mission concepts have been studied in detail, with emphasis on orbit design and resulting spatial-temporal ground track pattern, enhances processing and parameterization strategies, and improved post-processing/filtering strategies. Promising candidates for a next-generation gravity mission are double-pair and multi-pair constellations of GRACE/GRACE-FO-type satellites, as they are currently jointly studied by ESA and NASA. An alternative concept is high-precision ranging between high- and low-flying satellites. Since such a constellation observes mainly the radial component of gravity-induced orbit perturbations, the error structure is close to isotropic, which significantly reduces artefacts of along-track ranging formations. This high-low concept was proposed as ESA Earth Explorer 10 mission MOBILE and is currently further studies under the name MARVEL by the French space agency. Additionally, we evaluate the potential of a hybridization of electro-static and cold-atom accelerometers in order to improve the accelerometer performance in the low-frequency range.</p><p>In this contribution, based on full-fledged numerical closed-loop simulations with realistic error assumptions regarding their key payload, different mission constellations (in-line single-pair, Bender double-pair, multi-pairs, precise high-low tracking) are assessed and compared. Their overall performance, dealiasing potential, and recovery performance of short-periodic gravity signals are analyzed, in view of their capabilities to retrieve gravity field information with short latencies to be used for societally relevant service applications, such as water management, groundwater monitoring, and forecasting of droughts and floods.</p>

scholarly journals The control challenges for the Next Generation Gravity Mission

2013 ◽  
Author(s):  
Enrico Canuto ◽  
Marcello Buonocore ◽  
Stefano Cesare ◽  
Andrea Bacchetta ◽  
Benedicte Girouart ◽  
...  
Keyword(s):  
Next Generation ◽  
Gravity Mission

scholarly journals On Earthquake Detectability by the Next-Generation Gravity Mission

2020 ◽  
Vol 41 (5) ◽  
pp. 1049-1074 ◽  
Author(s):  
Gabriele Cambiotti ◽  
Karim Douch ◽  
Stefano Cesare ◽  
Roger Haagmans ◽  
Nicolas Sneeuw ◽  
...  
Keyword(s):  
Next Generation ◽  
Gravity Mission

Control Propellant Minimization for the Next Generation Gravity Mission

2019 ◽  
pp. 1-32
Author(s):  
Alberto Anselmi ◽  
Stefano Cesare ◽  
Sabrina Dionisio ◽  
Giorgio Fasano ◽  
Luca Massotti
Keyword(s):  
Next Generation ◽  
Gravity Mission

scholarly journals Embedded model control GNC for the Next Generation Gravity Mission

2017 ◽  
Vol 140 ◽  
pp. 497-508 ◽  
Author(s):  
Luigi Colangelo ◽  
Luca Massotti ◽  
Enrico Canuto ◽  
Carlo Novara
Keyword(s):  
Next Generation ◽  
Model Control ◽  
Embedded Model ◽  
Gravity Mission

The Results of the AOCS Solutions and Technologies study for the Next Generation Gravity Mission

2015 ◽  
Author(s):  
Andrea Bacchetta ◽  
Marcello Buonocore ◽  
Stefano Cesare ◽  
Sabrina Dionisio ◽  
Manlio Parisch ◽  
...  
Keyword(s):  
Next Generation ◽  
Gravity Mission

The Next Generation Gravity Mission and the qualification of the indium-fed mN-FEEP thruster

2021 ◽  
Author(s):  
L. Massotti ◽  
J. Gonzalez del Amo ◽  
P. Silvestrin ◽  
D. Krejci ◽  
A. Reissner ◽  
...  
Keyword(s):  
Next Generation ◽  
Gravity Mission

The Innovative Acquisition and Pointing Metrology for Next Generation Gravity Mission

2021 ◽  
Author(s):  
Luciana Bonino ◽  
Stefano Cesare ◽  
Bruno Leone ◽  
Luca Massotti ◽  
Marco Pisani ◽  
...  
Keyword(s):  
Next Generation ◽  
Gravity Mission
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