A structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systems

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.

Bibliographic Details
Main Author: Elias, Laila Mireille, 1977-
Other Authors: David W. Wallace.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2013
Subjects:
Online Access:http://hdl.handle.net/1721.1/81563
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author Elias, Laila Mireille, 1977-
author2 David W. Wallace.
author_facet David W. Wallace.
Elias, Laila Mireille, 1977-
author_sort Elias, Laila Mireille, 1977-
collection MIT
description Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.
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institution Massachusetts Institute of Technology
language eng
last_indexed 2024-09-23T10:09:51Z
publishDate 2013
publisher Massachusetts Institute of Technology
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spelling mit-1721.1/815632019-04-11T11:34:47Z A structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systems Coupled reaction wheel and spacecraft structural modeling via impedance measurement techniques Elias, Laila Mireille, 1977- David W. Wallace. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001. Includes bibliographical references (leaves 113-114). by Laila Mireille Elias. S.M. 2013-10-24T17:29:03Z 2013-10-24T17:29:03Z 2001 2001 Thesis http://hdl.handle.net/1721.1/81563 49870926 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 114 leaves application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics.
Elias, Laila Mireille, 1977-
A structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systems
title A structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systems
title_full A structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systems
title_fullStr A structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systems
title_full_unstemmed A structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systems
title_short A structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systems
title_sort structurally coupled disturbance analysis method using dynamic mass measurement techniques with application to spacecraft reaction wheel systems
topic Aeronautics and Astronautics.
url http://hdl.handle.net/1721.1/81563
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AT eliaslailamireille1977 coupledreactionwheelandspacecraftstructuralmodelingviaimpedancemeasurementtechniques
AT eliaslailamireille1977 structurallycoupleddisturbanceanalysismethodusingdynamicmassmeasurementtechniqueswithapplicationtospacecraftreactionwheelsystems