NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Model Reduction for Control System DesignAn approach and a technique for effectively obtaining reduced order mathematical models of a given large order model for the purposes of synthesis, analysis and implementation of control systems is developed. This approach involves the use of an error criterion which is the H-infinity norm of a frequency weighted error between the full and reduced order models. The weightings are chosen to take into account the purpose for which the reduced order model is intended. A previously unknown error bound in the H-infinity norm for reduced order models obtained from internally balanced realizations was obtained. This motivated further development of the balancing technique to include the frequency dependent weightings. This resulted in the frequency weighted balanced realization and a new model reduction technique. Two approaches to designing reduced order controllers were developed. The first involves reducing the order of a high order controller with an appropriate weighting. The second involves linear quadratic Gaussian synthesis based on a reduced order model obtained with an appropriate weighting.
Document ID
19850014087
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Enns, D. F.
(Stanford Univ. CA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-170417
NAS 1.26:170417
Accession Number
85N22398
Funding Number(s)
PROJECT: RTOP 505-34-01
CONTRACT_GRANT: NAG2-223
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available