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Bending feedback control Final reportApplication of quadratic optimal control, least squares state, and parameter estimation to stability and control of flexible launch vehicle
Document ID
19660022830
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Waymeyer, W. K. (Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Electronics
Report/Patent Number
DAC-59275
NASA-CR-76557
Report Number: DAC-59275
Report Number: NASA-CR-76557
Accession Number
66N32120
Funding Number(s)
CONTRACT_GRANT: NAS8-20087
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
OPTIMAL CONTROL
LAUNCH VEHICLE
STABILITY AND CONTROL
LEAST SQUARES METHOD

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