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Optimal piezo-actuator sizes and locations for a frame structure under bending load uncertainty are determined with the objective of minimizing the deflection under worst case of loading.
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The objectives are to minimize the deflection due to the prestress or to minimize ordinary compliance.
The basic control problem is to minimize the deflection and the velocity of displacements in a given period of time with the minimum possible expenditure of force.
Therefore, the present study focuses to optimize a typical FPCB electronic in order to minimize the deflection and stress induced in the system.
In minimizing the maximum deflection, the position of the maximum deflection from a previous iteration is used as the next one.
Optimal induced strain actuator sizes for an L-shaped laminated frame are determined under deterministic and uncertain loads with the objective of minimizing the tip deflection.
The bending moments generated by the induced strain actuators control the deflection in order to minimize the maximum deflection.
The optimum transverse core strength is determined for minimizing the back face deflection or support reactions at a given blast impulse.
The bending moments generated by the piezo-actuators are used for deflection control, i.e., to minimize the maximum deflection.
More specifically, we deal with finding the best way of mixing fixed amounts of two different elastic materials, so as to minimize the tip deflection of a cantilever beam loaded on its free extreme under the assumption of large deflections.
Based on the analytical deflection expression, necessary conditions are derived for the optimal values of segmental lengths and thicknesses that minimize the maximum deflection of stepped circular plates of a given volume.
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