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Author Osborne, R.C. ♦ Adams, R.J. ♦ Hsu, C.S. ♦ Banda, S.S.
Source IEEE Xplore Digital Library
Content type Text
Publisher Institute of Electrical and Electronics Engineers, Inc. (IEEE)
File Format PDF
Copyright Year ©1994
Language English
Subject Domain (in DDC) Technology ♦ Engineering & allied operations ♦ Other branches of engineering
Subject Keyword Aerospace control ♦ Control systems ♦ Riccati equations ♦ Design methodology ♦ Military aircraft ♦ Sufficient conditions ♦ Robust stability ♦ Eigenvalues and eigenfunctions ♦ Bridges ♦ Performance loss
Abstract A recently introduced method for designing H/sub /spl infin// compensators based on minimal-order observers is considered for an aircraft control problem. The purpose of this paper is to bridge the gap between theory and application by presenting a practical utilization of a new design approach. Manual flight control systems for the lateral axis of a fighter aircraft are developed using both full-order and reduced-order compensators and the results are compared. It is demonstrated that this method can be used to directly design reduced-order compensators which result in a system satisfying a closed-loop H/sub /spl infin// bound.<<ETX>>
Description Author affiliation: Flight Dynamics Directorate, Wright Lab., Wright-Patterson AFB, OH, USA (Osborne, R.C.; Adams, R.J.; Hsu, C.S.; Banda, S.S.)
ISBN 0780318722
Educational Role Student ♦ Teacher
Age Range above 22 year
Educational Use Research ♦ Reading
Education Level UG and PG
Learning Resource Type Article
Publisher Date 1993-09-13
Rights Holder Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Size (in Bytes) 452.15 kB
Page Count 6
Starting Page 853
Ending Page 858

Source: IEEE Xplore Digital Library