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 |
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| 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
Young, J-S., & Lin, C. E. (1992). Refined H∞ controller design for rotorcraft flight control. In Proceedings of the American Control Conference (Vol. 2, pp. 1523-1528). Publ by American Automatic Control Council.