Adaptive output feedback control methodology: Theory and practical implementation aspects

Moshe Idan, Anthony J. Calise, Naira Hovakimyan

Research output: Contribution to journalArticle

Abstract

Theoretical and practical implementation aspects of adaptive output feedback control method were analyzed. The method was found useful for applications in which, part of the system dynamics, actuator dynamics were nearly linear with relatively known characteristics. The controller synthesis included the proposed feedback linearization scheme coupled with a linear compensator design and adaptive NN-based element used to reduce the effect of model inversion error. It was suggested that open-loop system dynamics can be incorporated in the design through the proposed linearization procedure.

Original languageEnglish (US)
Pages (from-to)710-715
Number of pages6
JournalJournal of Guidance, Control, and Dynamics
Volume27
Issue number4
DOIs
StatePublished - Jan 1 2004

Fingerprint

Output Feedback Control
feedback control
Control theory
System Dynamics
Feedback control
Dynamical systems
methodology
linearization
Feedback Linearization
Feedback linearization
Methodology
output
Compensator
Linearization
Actuator
Inversion
Actuators
compensators
Synthesis
Controller

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Aerospace Engineering
  • Space and Planetary Science
  • Electrical and Electronic Engineering
  • Applied Mathematics

Cite this

Adaptive output feedback control methodology : Theory and practical implementation aspects. / Idan, Moshe; Calise, Anthony J.; Hovakimyan, Naira.

In: Journal of Guidance, Control, and Dynamics, Vol. 27, No. 4, 01.01.2004, p. 710-715.

Research output: Contribution to journalArticle

@article{a177bcac87b54123a3fea6c6e5870308,
title = "Adaptive output feedback control methodology: Theory and practical implementation aspects",
abstract = "Theoretical and practical implementation aspects of adaptive output feedback control method were analyzed. The method was found useful for applications in which, part of the system dynamics, actuator dynamics were nearly linear with relatively known characteristics. The controller synthesis included the proposed feedback linearization scheme coupled with a linear compensator design and adaptive NN-based element used to reduce the effect of model inversion error. It was suggested that open-loop system dynamics can be incorporated in the design through the proposed linearization procedure.",
author = "Moshe Idan and Calise, {Anthony J.} and Naira Hovakimyan",
year = "2004",
month = "1",
day = "1",
doi = "10.2514/1.11166",
language = "English (US)",
volume = "27",
pages = "710--715",
journal = "Journal of Guidance, Control, and Dynamics",
issn = "0731-5090",
publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",
number = "4",

}

TY - JOUR

T1 - Adaptive output feedback control methodology

T2 - Theory and practical implementation aspects

AU - Idan, Moshe

AU - Calise, Anthony J.

AU - Hovakimyan, Naira

PY - 2004/1/1

Y1 - 2004/1/1

N2 - Theoretical and practical implementation aspects of adaptive output feedback control method were analyzed. The method was found useful for applications in which, part of the system dynamics, actuator dynamics were nearly linear with relatively known characteristics. The controller synthesis included the proposed feedback linearization scheme coupled with a linear compensator design and adaptive NN-based element used to reduce the effect of model inversion error. It was suggested that open-loop system dynamics can be incorporated in the design through the proposed linearization procedure.

AB - Theoretical and practical implementation aspects of adaptive output feedback control method were analyzed. The method was found useful for applications in which, part of the system dynamics, actuator dynamics were nearly linear with relatively known characteristics. The controller synthesis included the proposed feedback linearization scheme coupled with a linear compensator design and adaptive NN-based element used to reduce the effect of model inversion error. It was suggested that open-loop system dynamics can be incorporated in the design through the proposed linearization procedure.

UR - http://www.scopus.com/inward/record.url?scp=3843071985&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=3843071985&partnerID=8YFLogxK

U2 - 10.2514/1.11166

DO - 10.2514/1.11166

M3 - Article

AN - SCOPUS:3843071985

VL - 27

SP - 710

EP - 715

JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

SN - 0731-5090

IS - 4

ER -