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Maneuvering and vibration control of flexible spacecraftEquations of motion, control strategy, perturbation, rigid-body maneuvers, quasi-modal equations, and vibration control are discussed for flexible spacecraft.
Document ID
19870013301
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Meirovitch, L. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Quinn, R. D. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA. Marshall Space Flight Center Structural Dynamics and Control Interaction of Flexible Structures
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N22734
Funding Number(s)
CONTRACT_GRANT: NAG1-225
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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