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Abstract

The combined system consisting of the baseline flexible structure modified by the system of active controllers is considered as a unified dynamical system. Techniques based on computer algebra are used to derive expressions for the transfer functions of the modified system, using the known transfer functions of the baseline flexible structure and the feedback gains of the active controller. The roots of the characteristic polynomial of this transfer function give the system resonant frequencies and damping parameters. Using the computer algebraic system MACSYMA, expressions for these parameters that are ex plicitly dependent on the output feedback gains of the active controller are presented. These results permit the parametric study of the placement of the resonant frequencies and damping parameters of the combined system as functions of the feedback gains. Numeri cal examples are used to illustrate the application of these results to the calculation of active controller feedback gains based on the requirement that certain modes have specified modal damping while the closed-loop frequencies remain unchanged.

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System Parameters of Output Feedback Controlled Flexible Structures

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