Modal Analysis Applied to Spacecraft Attitude Control

Aranda Almansa, Joaquín y Crespo, J. . (2007) Modal Analysis Applied to Spacecraft Attitude Control. AIAA Guidance, Navigation and Control Conference and Exhibit


Título Modal Analysis Applied to Spacecraft Attitude Control
Autor(es) Aranda Almansa, Joaquín
Crespo, J.
Palabras clave Modal
Analysis
Spacecraft
Attitude
Control
Editor(es) American Institute of Aeronautics and Astronautics
Fecha 2007-08-20
Formato text/html
Identificador bibliuned:595
Publicado en la Revista AIAA Guidance, Navigation and Control Conference and Exhibit
Idioma eng
Versión de la publicación publishedVersion
Tipo de recurso Article
Derechos de acceso y licencia http://creativecommons.org/licenses/by-nc-nd/4.0
info:eu-repo/semantics/openAccess
Tipo de acceso Acceso abierto
Notas adicionales spacecraft considered is a set of some flexible appendages flexible together with a rigid body. The flexible appendages considered are two solar panels attached to the main rigid bus. From the perspective of attitude control is interesting to analyse the motion repercussion between attitude maneuvers and solar panel deformation. Also is interesting to analyse the influence of solar panel deformation in misalignment in attitude motion. These type of subjects may be considered by means of a system modal analysis1. Modal analysis shall allow understanding deeply system performance necessaries to design and

 
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Creado: Tue, 13 Nov 2007, 12:10:20 CET