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Then, based on the proposed dynamics model, by constructing the modal filter, a robust H∞ independent modal space controller is designed and utilized to decouple the piezo-stage and deal with the unmodeled dynamics, disturbance, and hysteresis compensation error.
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We choose the modal filters as the state estimator to obtain the modal co-ordinates and modal velocities for the modal space control.
The independent modal space control is adopted for the active vibration control.
Optimal independent modal space control (IMSC) is applied for the design.
This method is compared with existing methods of modal space control, namely the independent modal space control (IMSC), and modified independent modal space control (MIMSC).
A new control algorithm modified independent modal space control (MIMSC) algorithm is proposed in this paper for eliminating the effect of modal control force on the uncontrolled modes.
The concept of independent modal space control is adopted, and the system is studied by the discrete-time model.
The performance of the independent modal space control (IMSC) algorithm for structural vibration control is examined in this paper.
According to this dynamics model, a robust independent modal space-fuzzy controller is designed for vibration control of a general MS, and the genetic optimization of some critical control parameters of fuzzy tuners is also presented.
An independent modal space fuzzy control technique for vibration control of earthquake-excited structures is presented.
A novel active force control strategy named modal space force control is proposed to solve these problems.
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