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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
19660059585
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Frosch, J. A.
Vallely, D. P.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Space Vehicles
Accession Number
66A38875
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT CONTROL
ATTITUDE CONTROL
SATURN V LAUNCH VEHICLE
AERODYNAMIC STABILITY

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