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Earthquake Engineering Research - HKU Libraries - The University ...

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211<br />

To examine the effect of the control forces on the uncontrolled modes, residual modes can be written<br />

^R(^= : A R w R (t) J rB R f(t) + E R x g (12)<br />

where W R is a residual state vector by uncontrolled modes. Substituting Eq. (10) into Eq. (4) and<br />

considering Eq. (12), we obtain<br />

w c (r) = A c w c (t)-B c K c w c (t) + E c x g} w R (t)-A R w R (t)-B R K c w c (f) + E R x (13)<br />

Moreover, substituting Eqs. (10) and (11) into Eq. (8), we can write the observer equation in the form<br />

* c (t) = (Ac - B C K C )>v c (r) + LC C (w c (t) - w c (r)) + LC R W R (r) + E c x g (14)<br />

<strong>The</strong> error vector is defined such as e c (t) = w c (t) - w c (t). <strong>The</strong>n the Equations can be written in the<br />

matrix form<br />

A C -B C K C 0<br />

0<br />

~B C K C<br />

— BffK r<br />

(15)<br />

LC R A C -LC C<br />

Note that the term -B^Kc in Eq. (15) is responsible for the excitation of the residual modes by the<br />

control forces and is known as control spilloveralas. If CR is zeros, which means the sensor signal only<br />

include controlled modes, the term -B&Kc has no effect on the eigenvalues of the closed-loop system.<br />

Hence, we conclude that control spillover cannot destabilize the system, although it can cause some<br />

degradation in the system performance. Normally, however, the above system can not satisfy the<br />

separate principle because the term LC# affects eigenvalues of the controlled system by the observer.<br />

This effect is known as observation spillover and can produce instability in the residual modes.<br />

However, a small amount of damping inherent in the structure is often sufficient to overcome the<br />

observation spillover effect. At any rate, observation spillover can be eliminated if the sensor signals<br />

are prefiltered so as to screen out the contribution of the uncontrolled modes (Meirovitch, 1990)<br />

Numerical Example<br />

To evaluate the proposed modal control scheme for use with the MR damper, a numerical example is<br />

considered in which a model of a six-story building is controlled with four MR dampers (Fig. 1). This<br />

numerical example is the same with that of Jansen and Dyke (2000) and is adopted for direct<br />

comparisons between the proposed modal control scheme and other control algorithms. In simulation,<br />

the model of the structure is subjected to the NS component of the 1940 El Centro earthquake. Because

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