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Research in and application of modern automatic control theory to nuclear rocket dynamics and control, volume I Semiannual status reportLinear optimal feedback control theory for nuclear rocket dynamics and control problems
Document ID
19660010593
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Melsa, J. L. (Arizona Univ. Tucson, AZ, United States)
Nordal, D. M. (Arizona Univ. Tucson, AZ, United States)
Secker, P. A. (Arizona Univ. Tucson, AZ, United States)
Shultz, D. G. (Arizona Univ. Tucson, AZ, United States)
Slivinsky, C. R. (Arizona Univ. Tucson, AZ, United States)
Weaver, L. E. (Arizona Univ. Tucson, AZ, United States)
Date Acquired
August 3, 2013
Publication Date
February 1, 1966
Subject Category
Electronics
Report/Patent Number
NASA-CR-70862
Report Number: NASA-CR-70862
Accession Number
66N19882
Funding Number(s)
CONTRACT_GRANT: NSG-490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIAPUNOV FUNCTION
MATHEMATICAL MODEL
LINEAR TRANSFORMATION
TIME OPTIMAL CONTROL
AUTOMATIC CONTROL
FEEDBACK CONTROL SYSTEM
ALGEBRA

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