Finite memory approximations for a singular neutral system arising in aeroelasticity

Author

Cliff, E.M. ; Herdman, Terry L. ; Turi, Janos

Author_Institution

Virginia Polytech. Inst. & State Univ., Blacksburg, VA, USA

fYear

1991

fDate

11-13 Dec 1991

Firstpage

3014

Abstract

An approach to finding numerical solutions of certain initial-value problems involving infinite-delay singular neutral differential equations is presented. Such systems arise in the study of the motions of airfoils placed in 2D unsteady flows and play an important role in controller design for aircraft flutter suppression. The two-step procedure starts with truncating the infinite-delay term and is dependent on the specified initial data. For the second step, a fully discretized approximation scheme that can be used to find approximate solutions for the associated finite delay equation is outlined

Keywords

aircraft control; control system synthesis; delays; elasticity; initial value problems; 2D unsteady flows; aeroelasticity; aircraft flutter suppression; airfoils; controller design; finite memory approximations; infinite-delay singular neutral differential equations; initial-value problems; numerical solutions; singular neutral system; term truncation; Aerodynamics; Aerospace control; Aerospace engineering; Aircraft; Automotive components; Contracts; Control systems; Delay; Delay systems; Differential equations; History; Mathematical model; Mathematics; Motion control; Oceans;

fLanguage

English

Publisher

ieee

Conference_Titel

Decision and Control, 1991., Proceedings of the 30th IEEE Conference on

Conference_Location

Brighton

Print_ISBN

0-7803-0450-0

Type

conf

DOI

10.1109/CDC.1991.261099

Filename

261099