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The highly coupled system - A general approach to the passive attitude stabilization of space vehiclesPassive attitude control and stability for space vehicles with nonsymmetrical mass distribution, by means of inertial coupling between degrees of freedom
Document ID
19660019927
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Merrick, V. K. (NASA Ames Research Center Moffett Field, CA, United States)
Moran, F. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1966
Subject Category
Navigation
Report/Patent Number
NASA-TN-D-3480
Report Number: NASA-TN-D-3480
Accession Number
66N29217
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MASS DISTRIBUTION
GRAVITY
STABILITY AND CONTROL
INERTIA
ATTITUDE CONTROL
SPACE VEHICLE
DEGREE OF FREEDOM

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