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Pizarro Rubio, A. and Pelaez Alvarez, Jesus (2008). On the attitude propagation of an axisymmetric satellite. In: "18th Space Flight Mechanics Meetings", 27-31 ene 2008, Galveston. ISBN 978-0-87703-544-2. pp. 535-554.
Title: | On the attitude propagation of an axisymmetric satellite |
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Author/s: |
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Item Type: | Presentation at Congress or Conference (Article) |
Event Title: | 18th Space Flight Mechanics Meetings |
Event Dates: | 27-31 ene 2008 |
Event Location: | Galveston |
Title of Book: | Spaceflight Mechanics 2008. Advances in the Astronautical Sciences |
Título de Revista/Publicación: | Spaceflight Mechanics Meeting 2008 . Advances in the Astronautical Sciences |
Date: | 2008 |
ISBN: | 978-0-87703-544-2 |
ISSN: | 978-0-87703-544-2. |
Volume: | 130 |
Subjects: | |
Faculty: | E.T.S.I. Aeronáuticos (UPM) |
Department: | Física Aplicada a la Ingeniería Aeronáutica [hasta 2014] |
Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
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This paper describes the method developed in the Group of Tether Dynamics of the UPM to gain accuracy in the numerical propagation of the attitude dynamics of a rigid axisymmetric spacecraft. We use a perturbation method which takes as unperturbed problem the Euler-Poinsot case (torque free). The perturbed problem provides the motion forced by non-vanishing external torques. Some numerical comparisons have been carried out to check the kindness of the procedure taking as forced motion some particular case of the Lagrange top, whose analytical solution permits an easy determination of the errors made in the numerical description of the motion.
Type | Code | Acronym | Leader | Title |
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Government of Spain | ESP2004-04376 | Unspecified | Unspecified | Dynamics of satellite orbit descent/raise using elctrodynamics tethers |
Item ID: | 52061 |
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DC Identifier: | https://oa.upm.es/52061/ |
OAI Identifier: | oai:oa.upm.es:52061 |
Deposited by: | Memoria Investigacion |
Deposited on: | 21 Mar 2019 11:45 |
Last Modified: | 21 Mar 2019 11:45 |