Refined H controller design for rotorcraft flight control

Jieh-Shian Young, Chin E. Lin

研究成果: Conference contribution

2 引文 斯高帕斯(Scopus)

摘要

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.

原文English
主出版物標題Proceedings of the American Control Conference
發行者Publ by American Automatic Control Council
頁面1523-1528
頁數6
2
ISBN(列印)0780302109
出版狀態Published - 1992 十二月 1
事件Proceedings of the 1992 American Control Conference - Chicago, IL, USA
持續時間: 1992 六月 241992 六月 26

Other

OtherProceedings of the 1992 American Control Conference
城市Chicago, IL, USA
期間92-06-2492-06-26

    指紋

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering

引用此

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