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

Jieh Shian Young, Chin E. Lin

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

An approach to refine H-optimal controller for the 4-block H control problem is proposed. The Hnorm 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 languageEnglish
Title of host publicationProceedings of the 1st IEEE Conference on Control Applications, CCA 1992
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages818-824
Number of pages7
ISBN (Electronic)0780300475, 9780780300477
DOIs
Publication statusPublished - 1992 Jan 1
Event1st IEEE Conference on Control Applications, CCA 1992 - Dayton, United States
Duration: 1992 Sep 121992 Sep 16

Publication series

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

Conference

Conference1st IEEE Conference on Control Applications, CCA 1992
CountryUnited States
CityDayton
Period92-09-1292-09-16

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

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  • Cite this

    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