2019
DOI: 10.1093/mnras/stz2695
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The second-degree gravity coefficients of Phobos from two Mars Express flybys

Abstract: Several close spacecraft flybys of Phobos have been performed over the past 40 yr in order to determine the gravity field of this tiny Martian moon. In this work, the second-degree coefficients of the gravity field of Phobos were derived from the radio tracking data of two combined Mars Express flybys (2010 and 2013), by applying a least squares regularized inverse technique, that introduces as an a priori the gravity field retrieved from a shape model based on constant density hypothesis. A gravitational mass… Show more

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Cited by 20 publications
(27 citation statements)
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References 36 publications
(62 reference statements)
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“…From a technical viewpoint, it is a great challenge implementing a sampling method that complies with the above criteria in the absence of detailed information on the state of the regolith on the martian moons. Although gravity on the martian moons is much smaller than that of Mars or Earth's moon, it is several orders of magnitude larger than that of asteroids (Yang et al, 2019). This requires a more-tailored propulsion system directed towards the martian moons during touchdown and lift-off.…”
Section: Sampling Asteroids Versus Phobosmentioning
confidence: 99%
“…From a technical viewpoint, it is a great challenge implementing a sampling method that complies with the above criteria in the absence of detailed information on the state of the regolith on the martian moons. Although gravity on the martian moons is much smaller than that of Mars or Earth's moon, it is several orders of magnitude larger than that of asteroids (Yang et al, 2019). This requires a more-tailored propulsion system directed towards the martian moons during touchdown and lift-off.…”
Section: Sampling Asteroids Versus Phobosmentioning
confidence: 99%
“…MAGREAS uses an iterative weighted batch-least squares (WBLS) estimator to find an initial spacecraft state solution that results in the minimum residual variance for a given set of measurements. The performance of the MAGRREAS software was confirmed by cross-validation against the GEODYN II planetary spacecraft orbit determination and dynamic parameter solution platform, and it also has been employed to process MEX radio tracking data [ 31 , 32 ]. Moreover, a Monte Carlo method was applied to validate the capability of image data for MEX precise orbit determination during the MEX Phobos flyby [ 33 ].…”
Section: Resultsmentioning
confidence: 99%
“…In addition to the nominal accuracy, the observation scheduling also repeats that of the A48, page 5 of 13 A&A 644, A48 (2020) All the POD simulations were performed using a stable version of Wuhan University Deep space Orbit determination and Gravity recovery System (WUDOGS), an in-house developed software. It has been used in Moon (Yan et al 2020;Liu et al 2020), Mars (Yan et al 2018;Yang et al 2019), Mercury , and asteroid missions (Jin et al 2020).…”
Section: Concept and Significance Of A Pod Simulationmentioning
confidence: 99%