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Aircraft adaptive learning controlThe optimal control theory of stochastic linear systems is discussed in terms of the advantages of distributed-control systems, and the control of randomly-sampled systems. An optimal solution to longitudinal control is derived and applied to the F-8 DFBW aircraft. A randomly-sampled linear process model with additive process and noise is developed.
Document ID
19790010456
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lee, P. S. T. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Vanlandingham, H. F. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1979
Subject Category
Cybernetics
Report/Patent Number
NASA-CR-158119
Report Number: NASA-CR-158119
Accession Number
79N18627
Funding Number(s)
CONTRACT_GRANT: NSG-1239
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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