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Dynamics and control research applicable to Apollo extension systemsDisturbance envelope and experiment requirements for Apollo missions used to determine optimum control-moment gyro-jet system
Document ID
19670004915
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Keckler, C. R. (NASA Langley Research Center Hampton, VA, United States)
Kurzhals, P. R. (NASA Langley Research Center Hampton, VA, United States)
Piland, W. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 3, 2013
Publication Date
December 1, 1966
Subject Category
Space Vehicles
Accession Number
67N14244
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ATTITUDE CONTROL
EXPERIMENT DESIGN
OPTIMAL CONTROL
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