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NASA NTRS ยท 19820004207

Computational methods of robust controller design for aerodynamic flutter suppression

Abstract

The 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.

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BibTeXRIS

Anderson, L. R.. 1981-11-15. Computational methods of robust controller design for aerodynamic flutter suppression. https://ntrs.nasa.gov/citations/19820004207

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