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Development and testing of controller performance evaluation methodology for multi-input/multi-output digital control systemsDescribed here is the development and implementation of on-line, near real time controller performance evaluation (CPE) methods capability. Briefly discussed are the structure of data flow, the signal processing methods used to process the data, and the software developed to generate the transfer functions. This methodology is generic in nature and can be used in any type of multi-input/multi-output (MIMO) digital controller application, including digital flight control systems, digitally controlled spacecraft structures, and actively controlled wind tunnel models. Results of applying the CPE methodology to evaluate (in near real time) MIMO digital flutter suppression systems being tested on the Rockwell Active Flexible Wing (AFW) wind tunnel model are presented to demonstrate the CPE capability.
Document ID
19910013024
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pototzky, Anthony
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Wieseman, Carol
(NASA Langley Research Center Hampton, VA, United States)
Hoadley, Sherwood Tiffany
(NASA Langley Research Center Hampton, VA, United States)
Mukhopadhyay, Vivek
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Publication Information
Publication: Fourth NASA Workshop on Computational Control of Flexible Aerospace Systems, Part 2
Subject Category
Aircraft Stability And Control
Accession Number
91N22337
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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