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Use of simulation techniques to remove test- peculiar nonlinear effects from control system response.Simulation techniques to remove gimbal bearing looseness effect on frequency response and cross axis coupling of Saturn control system S-4B stage
Document ID
19680035964
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Curtis, H. S.
Hagstrom, C. T.
Date Acquired
August 4, 2013
Publication Date
January 1, 1967
Publication Information
Publisher: AMERICAN ASTRONAUTICAL SOCIETY,
Subject Category
Facilities, Research, And Support
Meeting Information
Meeting: NATIONAL SYMPOSIUM ON SATURN V/APOLLO AND BEYOND
Location: HUNTSVILLE, AL
Start Date: June 11, 1967
End Date: June 14, 1967
Accession Number
68A16936
Funding Number(s)
CONTRACT_GRANT: NAS7-101
Distribution Limits
Public
Copyright
Other

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