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On the dynamics of spacecraft with flexible, deployable and slewing appendages

Resource type
Thesis
Thesis type
(Thesis) Ph.D.
Date created
1993
Authors/Contributors
Author: Shen, Qianruo
Copyright statement
Copyright is held by the author.
Permissions
The author has not granted permission for the file to be printed nor for the text to be copied and pasted. If you would like a printable copy of this thesis, please contact summit-permissions@sfu.ca.
Scholarly level
Graduate student (PhD)
Supervisor or Senior Supervisor
Thesis advisor: Medi, V.J.
Language
English
Member of collection
Statistics and Actuarial Science Theses
Mathematics Theses
Download file Size
b1519694x.pdf 3.85 MB

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