论文信息 - Reduced-Order H^ Compensator Design for an Aircraft Control Problem

Reduced-Order H^ Compensator Design for an Aircraft Control Problem

A recently introduced method for designing //<» compensators based on minimal-order observers is considered for an aircraft control problem. The purpose of this paper is to bridge the gap between theory and application by presenting a practical utilization of a new design approach. Manual flight control systems for the lateral axis of a fighter aircraft are developed using both full-order and reduced-order compensators, and the results are compared. It is demonstrated that this method can be used to directly design reduced-order compensators that result in a system satisfying a closed-loop //« bound.

Richard Adams | Siva S. Banda | Chin S. Hsu | Robert C. Osborne

[1] H.H. Yeh,et al. H∞ compensator design with minimal order observers , 1993, 1993 American Control Conference.

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

[3] Richard J. Adams,et al. Robust flight control design using dynamic inversion and structured singular value synthesis , 1993, IEEE Trans. Control. Syst. Technol..

[4] William R. Perkins,et al. Design of reliable control systems , 1992 .

[5] K. Glover,et al. A state space approach to H ∞ optimal control , 1989 .

[6] William S. Levine,et al. An introduction to H/sub infinity / control system design , 1990, 29th IEEE Conference on Decision and Control.

[7] T. Nguyen,et al. Optimal disturbance rejection in missile autopilot design using projective controls , 1992, IEEE Control Systems.

[8] Rick H. Middleton,et al. Trade-offs in linear control system design , 1991, Autom..

[9] W. B. DeShetler,et al. On minimal order stabilization of multivariable plants , 1992, [1992] Proceedings of the 31st IEEE Conference on Decision and Control.