The Mercury Orbiter Radioscience Experiment (MORE) on-board the BepiColombo mission was designed to provide an accurate estimation of the gravity field and the rotational state of Mercury. The Mercury Planetary Orbiter (MPO) is equipped with on-board instrumentation that allows highly stable, multi-frequency radio links in X and Ka band in order to achieve range rate and range coherent two-way measurements accurate to 0.003 mm/s (at 1000 s integration time) and 20 cm, respectively. Precise trajectory reconstruction allows us to estimate accurately the spherical harmonic coefficients of the Hermean gravity field, at least up to degree 35, the tide and the rotational parameters (right ascension and declination of the pole and physical librations in longitude). The determination these parameters provides crucial information on the interior structure of the planet. A full numerical simulation of the radioscience orbit determination process has been carried out taking into account the data provided by the on-board Italian Spring Accelerometer (ISA). This allows us to realize a software version of a drag-free system. In this paper, we report on the results of these numerical simulations aiming at a realistic assessment of the attainable accuracy in the determination of the gravity field and the rotation of Mercury with the implementation of a pseudo drag-free orbit determination process.

Bepicolombo gravity and rotation experiment in a pseudo drag-free system / Cappuccio, P.; Di Ruscio, A.; Iess, L.; Mariani, M. J.. - (2020), pp. 1-12. (Intervento presentato al convegno AIAA Scitech Forum, 2020 tenutosi a USA, Orlando FL) [10.2514/6.2020-1095].

Bepicolombo gravity and rotation experiment in a pseudo drag-free system

Cappuccio P.
Membro del Collaboration Group
;
Di Ruscio A.
Membro del Collaboration Group
;
Iess L.
Membro del Collaboration Group
;
Mariani M. J.
Membro del Collaboration Group
2020

Abstract

The Mercury Orbiter Radioscience Experiment (MORE) on-board the BepiColombo mission was designed to provide an accurate estimation of the gravity field and the rotational state of Mercury. The Mercury Planetary Orbiter (MPO) is equipped with on-board instrumentation that allows highly stable, multi-frequency radio links in X and Ka band in order to achieve range rate and range coherent two-way measurements accurate to 0.003 mm/s (at 1000 s integration time) and 20 cm, respectively. Precise trajectory reconstruction allows us to estimate accurately the spherical harmonic coefficients of the Hermean gravity field, at least up to degree 35, the tide and the rotational parameters (right ascension and declination of the pole and physical librations in longitude). The determination these parameters provides crucial information on the interior structure of the planet. A full numerical simulation of the radioscience orbit determination process has been carried out taking into account the data provided by the on-board Italian Spring Accelerometer (ISA). This allows us to realize a software version of a drag-free system. In this paper, we report on the results of these numerical simulations aiming at a realistic assessment of the attainable accuracy in the determination of the gravity field and the rotation of Mercury with the implementation of a pseudo drag-free orbit determination process.
2020
AIAA Scitech Forum, 2020
space exploration; gravity field; radio science; planetary geodesy; aerospace engineering
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Bepicolombo gravity and rotation experiment in a pseudo drag-free system / Cappuccio, P.; Di Ruscio, A.; Iess, L.; Mariani, M. J.. - (2020), pp. 1-12. (Intervento presentato al convegno AIAA Scitech Forum, 2020 tenutosi a USA, Orlando FL) [10.2514/6.2020-1095].
File allegati a questo prodotto
File Dimensione Formato  
Cappuccio_bepicolombo-gravity-rotation_2020.pdf

solo gestori archivio

Tipologia: Versione editoriale (versione pubblicata con il layout dell'editore)
Licenza: Tutti i diritti riservati (All rights reserved)
Dimensione 822.3 kB
Formato Adobe PDF
822.3 kB Adobe PDF   Contatta l'autore

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1448908
Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus 11
  • ???jsp.display-item.citation.isi??? ND
social impact