Title :
Refined H∞ optimal approach to rotorcraft flight control-a simulation on time responses
Author :
Young, Jieh-Shian ; Lin, Chin E.
Author_Institution :
Chung San Inst. of Sci. & Technol., Tao-Yuan, Taiwan
Abstract :
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
Keywords :
aircraft control; control system synthesis; frequency-domain analysis; helicopters; optimal control; time-domain analysis; H∞-optimal controller; McMillan degree; aircraft control; frequency domain; helicopters; rotorcraft flight control; time domain; time responses; Aerospace simulation; Economic indicators; H infinity control; Optimal control; Time factors; Transfer functions; Vents;
Conference_Titel :
Control Applications, 1992., First IEEE Conference on
Conference_Location :
Dayton, OH
Print_ISBN :
0-7803-0047-5
DOI :
10.1109/CCA.1992.269742
