Output feedback design for aircraft with ill-conditioned dynamics
- 1 January 1983
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 1084-1087
- https://doi.org/10.1109/cdc.1983.269687
Abstract
Singular perturbation concepts are exploited to develop a procedure for designing a dynamic output feedback controller. It is assumed that the original system is ill-conditioned in the sense that the plant contains widely separated dynamics requiring stabilization, and that the measurements are composed of a linear combination of slow and fast variables. A two time scale design approach results which depends on two-way control spillover suppression. An application to active control of aircraft wing flutter modes is used to illustrate the design method.Keywords
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