Refined H                         
                        ∞
                                                 -optimal approach to rotorcraft flight control - A simulation on time responses

Jieh Shian Young; Chin-E. Lin

doi:10.1109/CCA.1992.269742

Refined H ^∞ -optimal approach to rotorcraft flight control - A simulation on time responses

Jieh Shian Young, Chin-E. Lin

研究成果: Conference contribution

1 引文斯高帕斯（Scopus）

摘要

An approach to refine H ^∞ -optimal controller for the 4-block H ^∞ control problem is proposed. The H ^∞ norm of the sub-layers can, therefore, be improved by this approach. Furthermore, a simulation concerning the rotorcraft flight control on time responses is provided. The simulation results bestow a promissing progress both in frequency domain and in the time domain without the inflation of the McMillan degree of the controller.

原文	English
主出版物標題	Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992
發行者	Institute of Electrical and Electronics Engineers Inc.
頁面	818-824
頁數	7
ISBN（電子）	0780300475, 9780780300477
DOIs	https://doi.org/10.1109/CCA.1992.269742
出版狀態	Published - 1992 一月 1
事件	1st IEEE Conference on Control Applications, CCA 1992 - Dayton, United States 持續時間: 1992 九月 12 → 1992 九月 16

出版系列

名字	Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992

Conference

Conference	1st IEEE Conference on Control Applications, CCA 1992
國家	United States
城市	Dayton
期間	92-09-12 → 92-09-16

All Science Journal Classification (ASJC) codes

Electrical and Electronic Engineering
Control and Optimization
Computer Science (miscellaneous)
Control and Systems Engineering
Aerospace Engineering
Industrial and Manufacturing Engineering

存取文件

10.1109/CCA.1992.269742

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引用此

Young, J. S., & Lin, C-E. (1992). Refined H ^∞ -optimal approach to rotorcraft flight control - A simulation on time responses 於 Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992 (頁 818-824). [269742] (Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCA.1992.269742

Young, Jieh Shian ; Lin, Chin-E. / Refined H ^∞ -optimal approach to rotorcraft flight control - A simulation on time responses Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992. Institute of Electrical and Electronics Engineers Inc., 1992. 頁 818-824 (Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992).

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abstract = " An approach to refine H ∞ -optimal controller for the 4-block H ∞ control problem is proposed. The H ∞ norm of the sub-layers can, therefore, be improved by this approach. Furthermore, a simulation concerning the rotorcraft flight control on time responses is provided. The simulation results bestow a promissing progress both in frequency domain and in the time domain without the inflation of the McMillan degree of the controller. ",

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Young, JS & Lin, C-E 1992, Refined H ^∞ -optimal approach to rotorcraft flight control - A simulation on time responses 於 Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992., 269742, Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992, Institute of Electrical and Electronics Engineers Inc., 頁 818-824, 1st IEEE Conference on Control Applications, CCA 1992, Dayton, United States, 92-09-12. https://doi.org/10.1109/CCA.1992.269742

Refined H ^∞ -optimal approach to rotorcraft flight control - A simulation on time responses . / Young, Jieh Shian; Lin, Chin-E.

Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992. Institute of Electrical and Electronics Engineers Inc., 1992. p. 818-824 269742 (Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992).

研究成果: Conference contribution

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AU - Young, Jieh Shian

AU - Lin, Chin-E.

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N2 - An approach to refine H ∞ -optimal controller for the 4-block H ∞ control problem is proposed. The H ∞ norm of the sub-layers can, therefore, be improved by this approach. Furthermore, a simulation concerning the rotorcraft flight control on time responses is provided. The simulation results bestow a promissing progress both in frequency domain and in the time domain without the inflation of the McMillan degree of the controller.

AB - An approach to refine H ∞ -optimal controller for the 4-block H ∞ control problem is proposed. The H ∞ norm of the sub-layers can, therefore, be improved by this approach. Furthermore, a simulation concerning the rotorcraft flight control on time responses is provided. The simulation results bestow a promissing progress both in frequency domain and in the time domain without the inflation of the McMillan degree of the controller.

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M3 - Conference contribution

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BT - Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992

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Young JS, Lin C-E. Refined H ^∞ -optimal approach to rotorcraft flight control - A simulation on time responses 於 Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992. Institute of Electrical and Electronics Engineers Inc. 1992. p. 818-824. 269742. (Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992). https://doi.org/10.1109/CCA.1992.269742