论文信息 - Application of modern control theory on a model of the X29 aircraft

Application of modern control theory on a model of the X29 aircraft

In this report, two different control strategies for a model of the X29 are presented. The first is based on the 11 design methodology and the second is based on the HE design methodology. The purpose here is to show that these methodologies make the design process quite systematic, and that the resulting controllers conform with our intiuition.

Decision Systems. | Munther A. Dahleh | David M Richards

[1] J. Pearson,et al. L^{1} -optimal compensators for continuous-time systems , 1987 .

[2] Munther A. Dahleh,et al. Optimal rejection of persistent disturbances, robust stability, and mixed sensitivity minimization , 1988 .

[3] P. Khargonekar,et al. State-space solutions to standard H2 and H∞ control problems , 1988, 1988 American Control Conference.

[4] M. Dahleh,et al. Minimization of a regulated response to a fixed input , 1988 .

[5] P. Khargonekar,et al. State-space solutions to standard H/sub 2/ and H/sub infinity / control problems , 1989 .

[6] J. Pearson,et al. l^{1} -optimal feedback controllers for MIMO discrete-time systems , 1987 .

[7] J. Pearson,et al. l1 - Optimal-Feedback Controllers for Discrete-Time Systems , 1986, 1986 American Control Conference.

[8] W. W. Quinn. Multivariable control of a forward swept wing aircraft. M.S. Thesis , 1986 .

[9] Munther A. Dahleh,et al. Time-varying vs. time-invariant compensation for rejection of persistent bounded disturbances and robust stabilization , 1989, Proceedings of the 28th IEEE Conference on Decision and Control,.

[10] M. Dahleh,et al. A necessary and sufficient condition for robust BIBO stability , 1988 .