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Gillmann Cedric Way M. J. Avice Guillaume Breuer Doris Golabek Gregor J. Höning Dennis Krissansen-Totton Joshua Lammer Helmut O’Rourke Joseph G. Persson Moa Plesa Ana-Catalina Salvador Arnaud Scherf Manuel Zolotov Mikhail Y. 《Space Science Reviews》2022,218(7):1-21
Space Science Reviews - The BepiColombo Environment Radiation Monitor (BERM) on board the European Space Agency’s Mercury Planetary Orbiter (MPO), is designed to measure the radiation... 相似文献
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Dehant Veronique Debaille Vinciane Dobos Vera Gaillard Fabrice Gillmann Cedric Goderis Steven Grenfell John Lee Höning Dennis Javaux Emmanuelle J. Karatekin Özgür Morbidelli Alessandro Noack Lena Rauer Heike Scherf Manuel Spohn Tilman Tackley Paul Van Hoolst Tim Wünnemann Kai 《Space Science Reviews》2019,215(6):1-48
Space Science Reviews - This paper reviews habitability conditions for a terrestrial planet from the point of view of geosciences. It addresses how interactions between the interior of a planet or... 相似文献
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Davide Loreggia Silvano Fineschi Gerardo Capobianco Alessandro Bemporad Marta Casti Federico Landini Gianalfredo Nicolini Luca Zangrilli Giuseppe Massone Vladimiro Noce Marco Romoli Luca Terenzi Gianluca Morgante Massimiliano Belluso Cedric Thizy Camille Galy Aline Hermans Pierre Franco Luciano Accatino 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(11):3793-3806
PROBA-3 is a space mission of the European Space Agency that will test, and validate metrology and control systems for autonomous formation flying of two independent satellites. PROBA-3 will operate in a High Elliptic Orbit and when approaching the apogee at 6·104 Km, the two spacecraft will align to realize a giant externally occulted coronagraph named ASPIICS, with the telescope on one satellite and the external occulter on the other one, at inter-satellite distance of 144.3 m. The formation will be maintained over 6 hrs across the apogee transit and during this time different validation operations will be performed to confirm the effectiveness of the formation flying metrology concept, the metrology control systems and algorithms, and the spacecraft manoeuvring. The observation of the Sun’s Corona in the field of view [1.08;3.0]RSun will represent the scientific tool to confirm the formation flying alignment. In this paper, we review the mission concept and we describe the Shadow Position Sensors (SPS), one of the metrological systems designed to provide high accuracy (sub-millimetre level) absolute and relative alignment measurement of the formation flying. The metrology algorithm developed to convert the SPS measurements in lateral and longitudinal movement estimation is also described and the measurement budget summarized. 相似文献
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