Refined H controller design for rotorcraft flight control

Jieh Shian Young, Chin E. Lin

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

This paper presents an approach to refine H-optimal controller for the 4-block H control problem. The diagonalizing matrix pair which connects the successive layers is constructed. The second singular value of the compensated system can be analyzed and synthesized with a free parameter by the proposed approach which is implementable in computation with appropriate selection of diagonalizing matrix pair. The H-norm of the sub-layers can, therefore, be improved. Furthermore, an engineering application concerning the rotorcraft flight control is provided. The simulation results bestow a promising progress in frequency domain.

Original languageEnglish
Title of host publicationProceedings of the American Control Conference
PublisherPubl by American Automatic Control Council
Pages1523-1528
Number of pages6
ISBN (Print)0780302109, 9780780302105
DOIs
Publication statusPublished - 1992 Jan 1
EventProceedings of the 1992 American Control Conference - Chicago, IL, USA
Duration: 1992 Jun 241992 Jun 26

Publication series

NameProceedings of the American Control Conference
Volume2
ISSN (Print)0743-1619

Other

OtherProceedings of the 1992 American Control Conference
CityChicago, IL, USA
Period92-06-2492-06-26

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering

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  • Cite this

    Young, J. S., & Lin, C. E. (1992). Refined H controller design for rotorcraft flight control. In Proceedings of the American Control Conference (pp. 1523-1528). (Proceedings of the American Control Conference; Vol. 2). Publ by American Automatic Control Council. https://doi.org/10.23919/acc.1992.4792363