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

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2 Author(s)
Young, Jieh-Shian ; Chung San Inst. of Sci. & Technol., Tao-Yuan, Taiwan ; Lin, C.E.

An approach to refining an H∞-optimal controller for the four-block H∞ control problem is proposed. The H∞ norm of the sublayers can be improved by this approach. A simulation of the rotorcraft flight control on time responses is provided. The simulation results show promising progress both in the frequency domain and in the time domain without inflation of the McMillan degree of the controller

Published in:
Control Applications, 1992., First IEEE Conference on

Date of Conference: 13-16 Sep 1992

Page(s):
818 - 824 vol.2
Meeting Date :
13 Sep 1992-16 Sep 1992
Print ISBN:
0-7803-0047-5
INSPEC Accession Number:
4589894
Conference Location :
Dayton, OH
Digital Object Identifier :
10.1109/CCA.1992.269742
Product Type:
Conference Publications

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