TY - GEN
T1 - Refined H∞-optimal approach to rotorcraft flight control - A simulation on time responses
AU - Young, Jieh Shian
AU - Lin, Chin E.
PY - 1992/1/1
Y1 - 1992/1/1
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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U2 - 10.1109/CCA.1992.269742
DO - 10.1109/CCA.1992.269742
M3 - Conference contribution
AN - SCOPUS:33747859488
T3 - Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992
SP - 818
EP - 824
BT - Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 1st IEEE Conference on Control Applications, CCA 1992
Y2 - 12 September 1992 through 16 September 1992
ER -