Mothercraft-cubesat radio measurement for phobos survey
Mothercraft-cubesat radio measurement for phobos survey
The objective of this work is to investigate the application of radio link between the mothercraft and a CubeSat to the geodesy of Phobos. The origin of Martian moons (i.e. Phobos and Deimos) is still unknown. There are possibilities that they are ejected from Mars after an impact, or they are captured C-type asteroid. The knowledge of Phobos interior structure (e.g. homogeneous, porous, or fractured) will lead to better understanding towards its formation as well as the early solar system. The mothercraft and the CubeSat are flown in a safe high quasisatellite orbit (QSO) and a sustaining low QSO, respectively. Besides the Doppler measurement noise (0.1 mm/s), the ephemeris error of Phobos at least 200 m is found to be very disturbing for Phobos proximity operations. Nevertheless, the relative motion between the high QSO and the low three-dimensional QSO are resistant enough to reveal C20, C22, and to an accuracy of 0.3%, 1%, and 0.6% after one week. Such an accuracy can effectively constrain the moment of inertia as well as the interior structure of the target. The inter-sat radiometric measurement can also support the orbit determination of spacecraft with an accuracy of 240 m and 5 cm/s with respect to Phobos.
387-403
Chen, Hongru
8286469d-afe1-46e5-b107-694017de4d97
Rambaux, Nicolas
dbc7fcc9-fe7a-4f22-9288-de9eeabf14e2
Lainey, Valery
fa5aea68-6aa9-4433-a7ee-31071354bcca
Hestroffer, Daniel
06b8b68f-3a94-4f2e-b434-ce6822b08c71
28 January 2020
Chen, Hongru
8286469d-afe1-46e5-b107-694017de4d97
Rambaux, Nicolas
dbc7fcc9-fe7a-4f22-9288-de9eeabf14e2
Lainey, Valery
fa5aea68-6aa9-4433-a7ee-31071354bcca
Hestroffer, Daniel
06b8b68f-3a94-4f2e-b434-ce6822b08c71
Chen, Hongru, Rambaux, Nicolas, Lainey, Valery and Hestroffer, Daniel
(2020)
Mothercraft-cubesat radio measurement for phobos survey.
Graziani, Filippo
(ed.)
In 5th IAA Conference on University Satellite Missions and CubeSat Workshop, 2020.
vol. 173,
Univelt, Inc.
.
Record type:
Conference or Workshop Item
(Paper)
Abstract
The objective of this work is to investigate the application of radio link between the mothercraft and a CubeSat to the geodesy of Phobos. The origin of Martian moons (i.e. Phobos and Deimos) is still unknown. There are possibilities that they are ejected from Mars after an impact, or they are captured C-type asteroid. The knowledge of Phobos interior structure (e.g. homogeneous, porous, or fractured) will lead to better understanding towards its formation as well as the early solar system. The mothercraft and the CubeSat are flown in a safe high quasisatellite orbit (QSO) and a sustaining low QSO, respectively. Besides the Doppler measurement noise (0.1 mm/s), the ephemeris error of Phobos at least 200 m is found to be very disturbing for Phobos proximity operations. Nevertheless, the relative motion between the high QSO and the low three-dimensional QSO are resistant enough to reveal C20, C22, and to an accuracy of 0.3%, 1%, and 0.6% after one week. Such an accuracy can effectively constrain the moment of inertia as well as the interior structure of the target. The inter-sat radiometric measurement can also support the orbit determination of spacecraft with an accuracy of 240 m and 5 cm/s with respect to Phobos.
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Published date: 28 January 2020
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Publisher Copyright:
© 2020, Univelt Inc., All rights reserved.
Venue - Dates:
5th IAA Conference on University Satellite Missions and Cubesat Workshop, 2020, , Rome, Italy, 2020-01-28 - 2020-01-31
Identifiers
Local EPrints ID: 496995
URI: http://eprints.soton.ac.uk/id/eprint/496995
ISSN: 0065-3438
PURE UUID: c90d6f91-f0c9-4fc0-b308-e5ddfc6dae5a
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Date deposited: 09 Jan 2025 17:47
Last modified: 10 Jan 2025 03:19
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Contributors
Author:
Hongru Chen
Author:
Nicolas Rambaux
Author:
Valery Lainey
Author:
Daniel Hestroffer
Editor:
Filippo Graziani
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