By Haifeng Wang, Wenjuan Du
This publication offers the examine and improvement effects on strength platforms oscillations in 3 different types of analytical equipment. First is damping torque research which used to be proposed in 1960’s, extra constructed among 1980-1990, and favourite in undefined. moment is modal research which built among the 1980’s and 1990’s because the strongest technique. eventually the linearized equal-area criterion research that's proposed and constructed lately. The ebook covers 3 major different types of controllers: strength process Stabilizer (PSS), proof (Flexible AC Transmission structures) stabilizer, and ESS (Energy garage structures) stabilizer. The publication offers a scientific and targeted creation at the topic because the reference for purposes and educational examine.
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Extra resources for Analysis and Damping Control of Power System Low-frequency Oscillations
46) can be written in the following form ðAo À kIÞv ¼ 0 ð2:47Þ where I is an unity matrix. In order for Eq. 48) is the following polynomial equation if Ao is an M Â M matrix ðÀ1ÞM kM þ aMÀ1 kMÀ1 þ Á Á Á þ a1 k þ a0 ¼ 0 ð2:49Þ which is called the characteristic equation of state matrix Ao . The characteristic equation should have M solutions; that is, matrix Ao has M eigenvalues, if the dimension of matrix is M. For the ith eigenvalue of matrix Ao , ki , if a nonzero vector vi satisﬁes the equation Avi ¼ ki vi ; i ¼ 1; 2; .
Obviously, based on the discussion above, eigenvalues of Ac or modes of closed-loop system determine the stability of closed-loop system. From Eq. 68), it can be obtained that Ac ¼ Ao þ HðsÞbo cTo ð2:69Þ Denote a variable parameter of feedback controller as a. Thus, state matrix is a function of the parameter. Influence of the parameter on the ith mode of closed-loop system can be calculated by use of the following equation @ki @Ac ðaÞ @Hðki ; aÞ T T @Hðki ; aÞ vi ¼ wi bo co vi ¼ Ri ¼ wTi @a @a @a @a ð2:70Þ Hence, the residue measures how much the mode of closed-loop system is affected by the parameter of the controller.
59), it can have 2 z1 ð0Þek1 t 6 z2 ð0Þek2 t 6 X ¼ V6 .. 4 . 3 7 7 7 5 ð2:60Þ zn ð0ÞekM t Hence, time response of the xk ðtÞ; i ¼ 1; 2; . ; M, is as follows: kth state variable xk ðtÞ ¼ vk1 z1 ð0Þek1 t þ vk2 z2 ð0Þek2 t þ Á Á Á þ vkM zM ð0ÞekM t ¼ of M X the system, vki zi ð0Þeki t i¼1 ð2:61Þ Obviously, the time response of system state variables is decided by the eigenvalues of state matrix Ao . If there is one or more eigenvalues on the right-hand half of the complex plan (the real part of eigenvalue is equal to or greater than zero), the system is unstable.