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 |
| Volume | 2 |
| ISBN (Print) | 0780302109 |
| Publication status | Published - 1992 Dec 1 |
| Event | Proceedings of the 1992 American Control Conference - Chicago, IL, USA Duration: 1992 Jun 24 → 1992 Jun 26 |
Other
| Other | Proceedings of the 1992 American Control Conference |
|---|---|
| City | Chicago, IL, USA |
| Period | 92-06-24 → 92-06-26 |
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All Science Journal Classification (ASJC) codes
- Electrical and Electronic Engineering
Cite this
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Refined H∞ controller design for rotorcraft flight control. / Young, Jieh-Shian; Lin, Chin E.
Proceedings of the American Control Conference. Vol. 2 Publ by American Automatic Control Council, 1992. p. 1523-1528.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
TY - GEN
T1 - Refined H∞ controller design for rotorcraft flight control
AU - Young, Jieh-Shian
AU - Lin, Chin E.
PY - 1992/12/1
Y1 - 1992/12/1
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.
UR - http://www.scopus.com/inward/record.url?scp=0027037497&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0027037497&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:0027037497
SN - 0780302109
VL - 2
SP - 1523
EP - 1528
BT - Proceedings of the American Control Conference
PB - Publ by American Automatic Control Council
ER -