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Dynamics of a gravity-gradient stabilized flexible spacecraft

Author
Meirovitch, L.
Published
Aug 1, 1974.
Physical Description
1 electronic document
Additional Creators
Juang, J. N.
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
The dynamics of gravity-gradient stabilized flexible satellite in the neighborhood of a deformed equilibrium configuration are discussed. First the equilibrium configuration was determined by solving a set of nonlinear differential equations. Then stability of motion about the deformed equilibrium was tested by means of the Liapunov direct method. The natural frequencies of oscillation of the complete structure were calculated. The analysis is applicable to the RAE/B satellite.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19740027170.
Accession ID: 74N35283.
NASA-CR-2456.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15742487