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Control theory handbookMotion equations and basic control theory applied to stability and response analyses of flexible launch vehicle using unified coordinate system and notation
Document ID
19650017697
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Garner, D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
April 22, 1964
Subject Category
Electronics
Report/Patent Number
NASA-TM-X-53036
Report Number: NASA-TM-X-53036
Accession Number
65N27298
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COORDINATE SYSTEM
CONTROL SYSTEM
SPACECRAFT STABILITY
LAUNCH VEHICLE
MOTION EQUATION

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