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Effect of structural compliance-induced cross- axis coupling on the stability of a two-axis thrust vector attitude control system.Structural compliance induced cross axis coupling effect on gimballing system stability of rocket engine two-axis attitude TVC system
Document ID
19670039719
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Curtis, H. S.
Hagstrom, C. T.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 67-42
Report Number: AIAA PAPER 67-42
Accession Number
67A18448
Funding Number(s)
CONTRACT_GRANT: NAS7-101
Distribution Limits
Public
Copyright
Other
Keywords
GIMBALLED CONTROL
CROSS COUPLING
ROCKET ENGINE CONTROL
THRUST VECTOR CONTROL /TVC/
CONTROL STABILITY
ATTITUDE CONTROL

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