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.
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Format: | Thesis |
Language: | eng |
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Massachusetts Institute of Technology
2013
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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. |
first_indexed | 2024-09-23T10:09:51Z |
format | Thesis |
id | mit-1721.1/81563 |
institution | Massachusetts Institute of Technology |
language | eng |
last_indexed | 2024-09-23T10:09:51Z |
publishDate | 2013 |
publisher | Massachusetts Institute of Technology |
record_format | dspace |
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 |
work_keys_str_mv | AT eliaslailamireille1977 astructurallycoupleddisturbanceanalysismethodusingdynamicmassmeasurementtechniqueswithapplicationtospacecraftreactionwheelsystems AT eliaslailamireille1977 coupledreactionwheelandspacecraftstructuralmodelingviaimpedancemeasurementtechniques AT eliaslailamireille1977 structurallycoupleddisturbanceanalysismethodusingdynamicmassmeasurementtechniqueswithapplicationtospacecraftreactionwheelsystems |