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Saturn AS-501/S-IC flight control system design.Flight control system of Saturn V launch vehicle, discussing attitude/attitude-rate scheme, gain required and stability achieved
Document ID
19670056079
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Frosch, J. A.
Vallely, D. P.
Date Acquired
August 3, 2013
Publication Date
August 1, 1967
Publication Information
Publication: /AIAA/JACC GUIDANCE AND CONTROL CONFERENCE
Subject Category
Space Vehicles
Accession Number
67A34808
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT CONTROL
AERODYNAMIC STABILITY
ATTITUDE CONTROL
SATURN V LAUNCH VEHICLE

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