TY - GEN
T1 - Refined H∞ controller design for rotorcraft flight control
AU - Young, Jieh Shian
AU - Lin, Chin E.
PY - 1992/1/1
Y1 - 1992/1/1
N2 - This paper presents an approach to refine H∞-optimal controller for the 4-block H∞ control problem. The diagonalizing matrix pair which connects the successive layers is constructed. The second singular value of the compensated system can be analyzed and synthesized with a free parameter by the proposed approach which is implementable in computation with appropriate selection of diagonalizing matrix pair. The H∞-norm of the sub-layers can, therefore, be improved. Furthermore, an engineering application concerning the rotorcraft flight control is provided. The simulation results bestow a promising progress in frequency domain.
AB - This paper presents an approach to refine H∞-optimal controller for the 4-block H∞ control problem. The diagonalizing matrix pair which connects the successive layers is constructed. The second singular value of the compensated system can be analyzed and synthesized with a free parameter by the proposed approach which is implementable in computation with appropriate selection of diagonalizing matrix pair. The H∞-norm of the sub-layers can, therefore, be improved. Furthermore, an engineering application concerning the rotorcraft flight control is provided. The simulation results bestow a promising progress in frequency domain.
UR - http://www.scopus.com/inward/record.url?scp=0027037497&partnerID=8YFLogxK
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U2 - 10.23919/acc.1992.4792363
DO - 10.23919/acc.1992.4792363
M3 - Conference contribution
AN - SCOPUS:0027037497
SN - 0780302109
SN - 9780780302105
T3 - Proceedings of the American Control Conference
SP - 1523
EP - 1528
BT - Proceedings of the American Control Conference
PB - Publ by American Automatic Control Council
T2 - Proceedings of the 1992 American Control Conference
Y2 - 24 June 1992 through 26 June 1992
ER -