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Dive into the research topics where Constantine Houpis is active.

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Featured researches published by Constantine Houpis.


International Journal of Control | 1985

An algebraic approach to the time-optimal output regulator†

Charles D. Corsetti; Constantine Houpis

The time-optimal output regulator is considered for a special class of linear time-invariant discrete-time systems. It is shown that a simple state feedback law achieves time-optimal output regulator response in one sampling period. For a square system, the state feedback law always assigns the invariant zeros as closed-loop poles. For a non-square system, time-optimal regulator response is achieved even if the set of invariant zeros is empty. If the set of invariant zeros is not empty, the control law always assigns these zeros as closed-loop poles. The method of this paper, for the discrete system described by the state and output equations x(k + 1) = Ax(k) + Bu(k) and z(k) = Cx(k), does not require that A be invertible and that the open-loop system S(A, B, C) be state controllable. Furthermore, the only requirement is the existence of a right inverse for the matrix CB which is sufficient for output controllability.


ieee conference on aerospace and electronics | 1990

Stabilization of a flight control system with varying numbers of right half-plane poles and zeros

Isaac Horowitz; Constantine Houpis

Data for a linearized model of the STOL/maneuver technology demonstrator (SMTD) with stabiliser used to control pitch-rate are examined. Six flight conditions were considered, ranging from 0.1 to 0.9 Mach, and from zero to 40000 ft. The six cases comprised one with one right half-plane (RHP) zero and one RHP pole, two cases with two RHP poles, one case with one RHP zero and three RHP poles, and two cases with one RHP pole. The problem was to stabilize the system over this range of flight conditions by means of a single, fixed compensator, i.e. without any scheduling or identification. Quantitative feedback theory (QFT) was applied in a straightforward manner to obtain such a design with phase margins >or=50 degrees and gain margins >or=6 dB (only one case with 6 dB, the five others >or=20 dB). The technique is simple and systematic, with little cut-and-try. It can be applied by anyone with classical control background since the Nichols chart is the principal design tool. Time and frequency domain simulations are included.<<ETX>>


Archive | 1995

Linear control system analysis and design

John D'Azzo; Constantine Houpis; Richard L. Brunson


Automatica | 1999

Quantitative Feedback Theory: Fundamentals and Applications

Constantine Houpis; Steven Rasmussen


Archive | 1966

Feedback Control System Analysis and Synthesis

John D'Azzo; Constantine Houpis


Archive | 2003

Linear control system analysis and design with MATLAB

Constantine Houpis; Stuart Sheldon


Archive | 2012

Wind Energy Systems: Control Engineering Design

Mario Garcia-Sanz; Constantine Houpis


Archive | 2003

Linear Control System Analysis and Design : Fifth Edition, Revised and Expanded

John D'Azzo; Constantine Houpis; Stuart Sheldon


Archive | 2005

Quantitative Feedback Theory: Fundamentals and Applications, Second Edition

Constantine Houpis; Steven Rasmussen; Mario Garcia-Sanz


Archive | 2005

Introduction to QFT

Constantine Houpis; Steven Rasmussen; Mario Garcia-Sanz

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Mario Garcia-Sanz

Case Western Reserve University

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Isaac Horowitz

University of California

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Charles D. Corsetti

Air Force Institute of Technology

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I. M. Horowitz

Air Force Institute of Technology

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Richard L. Brunson

Air Force Institute of Technology

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Russel B. Miller

Air Force Institute of Technology

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