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Summary of the digital adaptive filter, digital polynomial filter and specification set control techniques applied to large launch vehiclesDigital polynomial and adaptive feedback control system techniques for large launch vehicle guidance, stability, and control
Document ID
19660013073
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Luedde, W. J. (McDonnell Aircraft Co. Saint Louis, MO, United States)
Zaborszky, J. (McDonnell Aircraft Co. Saint Louis, MO, United States)
Date Acquired
August 3, 2013
Publication Date
April 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
B897
NASA-CR-462
Report Number: B897
Report Number: NASA-CR-462
Accession Number
66N22362
Funding Number(s)
CONTRACT_GRANT: NAS8-11418
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LAUNCH VEHICLE
DIGITAL COMPUTER
ADAPTIVE CONTROL SYSTEM
STABILITY AND CONTROL
GUIDANCE AND CONTROL
FEEDBACK CONTROL SYSTEM

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