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On structural compliance-induced coupling in a thrust-vector control system.Structural compliance induced cross axis coupling effect on gimballing system stability of rocket engine two-axis attitude TVC system
Document ID
19670064180
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Curtis, H. S.
Hagstrom, C. T.
Date Acquired
August 3, 2013
Publication Date
November 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 67-42
Report Number: AIAA PAPER 67-42
Accession Number
67A42909
Funding Number(s)
CONTRACT_GRANT: NAS7-101
Distribution Limits
Public
Copyright
Other
Keywords
CONTROL STABILITY
THRUST VECTOR CONTROL /TVC/
ROCKET ENGINE CONTROL
GIMBALLED CONTROL
CROSS COUPLING
ATTITUDE CONTROL

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