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

Graduate Institute of Vehicle Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

1 Citation (Scopus)

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.

Original language	English
Title of host publication	Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	818-824
Number of pages	7
ISBN (Electronic)	0780300475, 9780780300477
DOIs	https://doi.org/10.1109/CCA.1992.269742
Publication status	Published - 1992 Jan 1
Event	1st IEEE Conference on Control Applications, CCA 1992 - Dayton, United States Duration: 1992 Sep 12 → 1992 Sep 16

Publication series

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

Conference

Conference	1st IEEE Conference on Control Applications, CCA 1992
Country	United States
City	Dayton
Period	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

Access to Document

10.1109/CCA.1992.269742

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Young, J. S., & Lin, C. E. (1992). Refined H^∞-optimal approach to rotorcraft flight control - A simulation on time responses. In Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992 (pp. 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

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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, CE 1992, Refined H^∞-optimal approach to rotorcraft flight control - A simulation on time responses. in 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., pp. 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).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

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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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Young JS, Lin CE. Refined H^∞-optimal approach to rotorcraft flight control - A simulation on time responses. In 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