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Computational methods of robust controller design for aerodynamic flutter suppressionThe development of Riccati iteration, a tool for the design and analysis of linear control systems is examined. First, Riccati iteration is applied to the problem of pole placement and order reduction in two-time scale control systems. Order reduction, yielding a good approximation to the original system, is demonstrated using a 16th order linear model of a turbofan engine. Next, a numerical method for solving the Riccati equation is presented and demonstrated for a set of eighth order random examples. A literature review of robust controller design methods follows which includes a number of methods for reducing the trajectory and performance index sensitivity in linear regulators. Lastly, robust controller design for large parameter variations is discussed.
Document ID
19820004207
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, L. R.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 4, 2013
Publication Date
November 15, 1981
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-164983
VPI-AERO-125
Report Number: NASA-CR-164983
Report Number: VPI-AERO-125
Accession Number
82N12080
Funding Number(s)
CONTRACT_GRANT: NAG1-80
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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