A structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systems
Name
49870926-MIT.pdf
Description
Full printable version
Size
11.36 MB
Format
Adobe PDF
Checksum (MD5)
19952ef6b78e6e9021f3fb9487cd4f60
Author(s)
Elias, Laila Mireille, 1977-
Advisor(s)
David W. Wallace.
Alternative Title
Coupled reaction wheel and spacecraft structural modeling via impedance measurement techniques
Date Issued
2001
Publisher
Massachusetts Institute of Technology
Description
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.
Includes bibliographical references (leaves 113-114).
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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copyright. They may be viewed from this source for any purpose, but
reproduction or distribution in any format is prohibited without written
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