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Sanjurjo Rivo, Manuel, Scheeres, D. and Peláez Álvarez, Jesús ORCID: https://orcid.org/0000-0001-9755-1674
(2014).
Jovian Capture of a Spacecraft with a Self-Balanced Electrodynamic Bare Tether.
"Journal of Spacecraft And Rockets", v. 51
(n. 5);
pp. 1401-1412.
ISSN 0022-4650.
https://doi.org/10.2514/1.A32550.
Title: | Jovian Capture of a Spacecraft with a Self-Balanced Electrodynamic Bare Tether |
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Author/s: |
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Item Type: | Article |
Título de Revista/Publicación: | Journal of Spacecraft And Rockets |
Date: | September 2014 |
ISSN: | 0022-4650 |
Volume: | 51 |
Subjects: | |
Faculty: | E.T.S.I. Aeronáuticos (UPM) |
Department: | Física Aplicada a las Ingenierías Aeronáutica y Naval |
Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
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This paper proposes and analyzes the use of a nonrotating tethered system for a direct capture in Jovian orbit using the electrodynamic force generated along the cable. A detailed dynamical model is developed showing a strong gravitational and electrodynamic coupling between the center of mass and the attitude motions. This paper shows the feasibility of a direct capture in Jovian orbit of a rigid tethered system preventing the tether from rotating. Additional mechanical–thermal requirements are explored, and preliminary operational limits are defined to complete the maneuver. In particular, to ensure that the system remains nonrotating, a nominal attitude profile for a self-balanced electrodynamic tether is proposed, as well as a simple feedback control.
Item ID: | 35185 |
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DC Identifier: | https://oa.upm.es/35185/ |
OAI Identifier: | oai:oa.upm.es:35185 |
DOI: | 10.2514/1.A32550 |
Official URL: | http://arc.aiaa.org/doi/abs/10.2514/1.A32550 |
Deposited by: | Memoria Investigacion |
Deposited on: | 27 May 2015 18:20 |
Last Modified: | 06 Feb 2023 12:21 |