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A method for partitioning centralized controllersThe notion of controller partitioning is described. Conditions are developed under which the input/output behavior of a multi-input multi-output centralized controller can be exactly matched by two separate subsystem controllers interconnected through output crossfeed. A systematic method is developed for determining a controller partitioning which best approximates the input/output behavior of the centralized controller for the general case when the exact matching conditions are not satisfied. The controller partitioning procedure is demonstrated for a centralized integrated flight/propulsion controller designed in a previous study.
Document ID
19910010820
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Schmidt, Phillip
(NASA Lewis Research Center Cleveland, OH., United States)
Garg, Sanjay
(Sverdrup Technology, Inc., Brook Park OH., United States)
Lorenzo, Carl F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1991
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:4276
NASA-TM-4276
E-5800
Accession Number
91N20133
Funding Number(s)
PROJECT: RTOP 505-62-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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