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Modal method for analysis of free rotations of spacecraft.Rotating spacecraft attitude changes due to energy dissipation from angular deformation treated by modal method
Document ID
19670051472
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Likins, P. W.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Publication Information
Publication: /AIAA/JACC GUIDANCE AND CONTROL CONFERENCE
Subject Category
Space Vehicles
Accession Number
67A30201
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT CONTROL
STRUCTURAL STABILITY
ATTITUDE CONTROL
ENERGY LOSS

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