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題名: Refined H∞ Controller Design for Rotorcraft Flight Control
作者: Young, Jieh-Shian;Lin, Chin E.
貢獻者: 車輛科技研究所
關鍵詞: 4-block HE-optimal control problem;Diagonalizing matrix pair;Inner extension;Maximal Schmidt pair;Sub-layers
日期: 1992
上傳時間: 2013-02-27T03:12:45Z
出版者: IEEE
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.
關聯: Proceedings of the American Control Conference, 2: 1523-1528
顯示於類別:[車輛科技研究所] 會議論文

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