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Development and testing of methodology for evaluating the performance of multi-input/multi-output digital control systemsA Controller Performance Evaluation (CPE) methodology for multi-input/multi-output digital control systems was developed and tested on an aeroelastic wind-tunnel model. Modern signal processing methods were used to implement control laws and to acquire time domain data of the whole system (controller and plant) from which appropriate transfer matrices of the control system could be generated. Matrix computational procedures were used to calculate singular values of return-difference matrices at the plant input and output points to evaluate the performance of the control system. The CPE procedures effectively identified potentially destabilizing controllers and confirmed the satisfactory performance of stabilizing ones.
Document ID
19900018383
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pototzky, Anthony S.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Wieseman, Carol D.
(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
August 1, 1990
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-102704
NAS 1.15:102704
Report Number: NASA-TM-102704
Report Number: NAS 1.15:102704
Meeting Information
Meeting: 1990 AIAA Guidance, Navigation, and Control Conference
Location: Portland, OR
Country: United States
Start Date: August 20, 1990
End Date: August 22, 1990
Accession Number
90N27699
Funding Number(s)
PROJECT: RTOP 505-63-21-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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