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An expert system to perform on-line controller restructuring for abrupt model changesThis paper presents the work in progress on an expert system utilized to tune and reconfigure airframe/engine control systems on-line in real time in response to structural or battle damage failures. The closed loop system is monitored constantly for changes in performance and structure, which detection prompts the expert system to select and apply a particular control restructuring algorithm based on the severity and type of damage. Control restructuring algorithms that have been implemented handle most failure cases involving actuator damage (control mixer) and many instances where the system dynamics are altered as well (modified control mixer).
Document ID
19910044843
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Litt, Jonathan
(NASA Lewis Research Center; U.S. Army, Propulsion Directorate, Cleveland OH, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aircraft Stability And Control
Accession Number
91A29466
Distribution Limits
Public
Copyright
Other

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