Refined H∞ controller design for rotorcraft flight control

Jieh Shian Young; Chin E. Lin

doi:10.23919/acc.1992.4792363

Refined H^∞ controller design for rotorcraft flight control

Jieh Shian Young, Chin E. Lin

Graduate Institute of Vehicle Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference 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 language	English
Title of host publication	Proceedings of the American Control Conference
Publisher	Publ by American Automatic Control Council
Pages	1523-1528
Number of pages	6
ISBN (Print)	0780302109, 9780780302105
DOIs	https://doi.org/10.23919/acc.1992.4792363
Publication status	Published - 1992 Jan 1
Event	Proceedings of the 1992 American Control Conference - Chicago, IL, USA Duration: 1992 Jun 24 → 1992 Jun 26

Publication series

Name	Proceedings of the American Control Conference
Volume	2
ISSN (Print)	0743-1619

Other

Other	Proceedings of the 1992 American Control Conference
City	Chicago, IL, USA
Period	92-06-24 → 92-06-26

All Science Journal Classification (ASJC) codes

Electrical and Electronic Engineering

Access to Document

10.23919/acc.1992.4792363

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title = "Refined H∞ controller design for rotorcraft flight control",

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.",

author = "Young, {Jieh Shian} and Lin, {Chin E.}",

year = "1992",

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series = "Proceedings of the American Control Conference",

publisher = "Publ by American Automatic Control Council",

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note = "Proceedings of the 1992 American Control Conference ; Conference date: 24-06-1992 Through 26-06-1992",

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Young, JS & Lin, CE 1992, Refined H^∞ controller design for rotorcraft flight control. in Proceedings of the American Control Conference. Proceedings of the American Control Conference, vol. 2, Publ by American Automatic Control Council, pp. 1523-1528, Proceedings of the 1992 American Control Conference, Chicago, IL, USA, 92-06-24. https://doi.org/10.23919/acc.1992.4792363

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AU - Young, Jieh Shian

AU - Lin, Chin E.

PY - 1992/1/1

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N2 - 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.

AB - 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.

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T3 - Proceedings of the American Control Conference

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BT - Proceedings of the American Control Conference

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