An Optimization Strategy For Reconfigurable Control Systems
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[1] Michael Athans,et al. The Matrix Minimum Principle , 1967, Inf. Control..
[2] D. Looze,et al. An automatic redesign approach for restructurable control systems , 1985, IEEE Control Systems Magazine.
[3] V. Gavito. Application of eigenstructure assignment to self reconfiguring aircraft MIMO controllers , 1987 .
[4] Panos J. AntsaklisDepartment. Design of Output Feedback Controllers for Robust Stability and Optimal Performance of Discrete-Time Systems , 1994 .
[5] D. Russell,et al. On stability with large parameter variations: Stemming from the direct method of Lyapunov , 1980 .
[6] Jerry M. Mendel,et al. On the design of optimal time-invariant compensators for linear stochastic time-invariant systems , 1975 .
[7] 위상규,et al. 저정 안정 항공기 제어를 위한 Eigenstructure Assignment , 1989 .
[8] N. E. Wu,et al. An approach to configuration of robust control systems for robust failure detection , 1993, Proceedings of 32nd IEEE Conference on Decision and Control.
[9] A.K. Caglayan,et al. Evaluation of a second generation reconfiguration strategy for aircraft flight control systems subjected to actuator failure/surface damage , 1988, Proceedings of the IEEE 1988 National Aerospace and Electronics Conference.
[10] J. R. Broussard,et al. Active Flutter Control using Discrete Optimal Constrained Dynamic Compensators , 1983, 1983 American Control Conference.
[11] P. Antsaklis,et al. Optimal design of robust controllers for uncertain discrete-time systems , 1996 .
[12] E.Y. Shapiro,et al. Eigenstructure Assignment for Linear Systems , 1983, IEEE Transactions on Aerospace and Electronic Systems.
[13] P. Antsaklis,et al. Stability of the pseudo-inverse method for reconfigurable control systems , 1991 .
[14] Jin Jiang,et al. Design of reconfigurable control systems using eigenstructure assignments , 1994 .
[15] Aaron J. Ostroff. Techniques for Accommodating Control Effector Failures on a Mildly Statically Unstable Airplane , 1985, 1985 American Control Conference.
[16] P. Howell. Full authority lateral-directional flight control system design using a reconfigurable control and adaptive learning network: a design proposal , 1992, [Proceedings 1992] The First IEEE Conference on Control Applications.
[17] H. Horisberger,et al. Solution of the optimal constant output feedback problem by conjugate gradients , 1974 .
[18] R. M. Hueschen,et al. Investigation of control law reconfigurations to accommodate a control element failure on a commercial airplane , 1984 .
[19] N. E. Wu. Reconfigurable control design: achieving stability robustness and failure tracking , 1993, Proceedings of 32nd IEEE Conference on Decision and Control.
[20] Marc Bodson,et al. Identification with modeling uncertainty and reconfigurable control , 1993, Proceedings of 32nd IEEE Conference on Decision and Control.
[21] John R. Broussard,et al. Application of precomputed control laws in a reconfigurable aircraft flight control system , 1989 .
[22] Meir Pachter,et al. On-line optimizing networks for reconfigurable control , 1993, Proceedings of 32nd IEEE Conference on Decision and Control.
[23] P. R. Chandler,et al. Self-repairing flight control system program overview , 1988, Proceedings of the IEEE 1988 National Aerospace and Electronics Conference.