Bifurcations in the attitude dynamics of a spacecraft in a gravity field
Arribas,M. (Universidad de Zaragoza) ; Casanova,D. (Universidad de Zaragoza) ; Elipe,A. (Universidad de Zaragoza) ; Palacios,M. (Universidad de Zaragoza)
Resumen: A normalized averaged (integrable) Hamiltonian approximation is used to study the attitude dynamics of a rigid body satellite in a gravity field, with an emphasis on bifurcations. The phase portrait is represented in a Mercator map and on a 3D sphere. Pitchfork bifurcations and degeneracies (a dense set of equilibria) are found.
Idioma: Inglés
DOI: 10.1016/j.mechrescom.2012.12.005
Año: 2013
Publicado en: MECHANICS RESEARCH COMMUNICATIONS 48 (2013), 59-65
ISSN: 0093-6413
Factor impacto JCR: 1.495 (2013)
Categ. JCR: MECHANICS rank: 54 / 139 = 0.388 (2013) - Q2 - T2
Tipo y forma: Article (PostPrint)
Área (Departamento): Área Matemática Aplicada (Dpto. Matemática Aplicada)
You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use. You may not use the material for commercial purposes. If you remix, transform, or build upon the material, you may not distribute the modified material.
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Idioma: Inglés
DOI: 10.1016/j.mechrescom.2012.12.005
Año: 2013
Publicado en: MECHANICS RESEARCH COMMUNICATIONS 48 (2013), 59-65
ISSN: 0093-6413
Factor impacto JCR: 1.495 (2013)
Categ. JCR: MECHANICS rank: 54 / 139 = 0.388 (2013) - Q2 - T2
Tipo y forma: Article (PostPrint)
Área (Departamento): Área Matemática Aplicada (Dpto. Matemática Aplicada)
You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use. You may not use the material for commercial purposes. If you remix, transform, or build upon the material, you may not distribute the modified material. Exportado de SIDERAL (2024-02-12-17:04:45)
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Record created 2024-02-12, last modified 2024-02-12