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An adaptive learning control system for aircraftA learning control system and its utilization as a flight control system for F-8 Digital Fly-By-Wire (DFBW) research aircraft is studied. The system has the ability to adjust a gain schedule to account for changing plant characteristics and to improve its performance and the plant's performance in the course of its own operation. Three subsystems are detailed: (1) the information acquisition subsystem which identifies the plant's parameters at a given operating condition; (2) the learning algorithm subsystem which relates the identified parameters to predetermined analytical expressions describing the behavior of the parameters over a range of operating conditions; and (3) the memory and control process subsystem which consists of the collection of updated coefficients (memory) and the derived control laws. Simulation experiments indicate that the learning control system is effective in compensating for parameter variations caused by changes in flight conditions.
Document ID
19780018023
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mekel, R.
(City Coll. of the City Univ. of New York NY, United States)
Nachmias, S.
(City Coll. of the City Univ. of New York NY, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Administration And Management
Report/Patent Number
NASA-CR-156930
Report Number: NASA-CR-156930
Accession Number
78N25966
Funding Number(s)
CONTRACT_GRANT: NSG-1169
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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