470 PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL
We have three poles at s - 0, -3, -5 and no finite zeros. Therefore, the missing
zeros arelocated at s -
As s + co, G(s) ~ 1~3 = O,i.e., G(s) has three zeros at s - c:o.
Consider
G(s) : s (5.134)
This system has a zero ats = 0 and a pole atinfinity because,as s ~ oo, G(s) + oo.
Similarly, G(s) -. l]s has a zero at infinity because G(s) -y 0 as s -+ oo.
5) Asymptotes. The asymptotes give the behavior of the root-locus as the param-
eter k approaches infinity. The point, ofintersection of the asymptotes with the real
axis uo (see Fig.5:15a) and the slopes ofthe asymptotes M at this point are given by
cro = Ppoles - E zeros
(5,135)
Fr P - r.z
M = tan np U. ~- (5.136)
where np and nz are the number of open-loop poles and zeros, respectively, and
n -. 0, :1:1, +2,.... The running index n gives the slopes of the asymptotes that
form the branches:of the root-locus as k -* oo.
/maginary axis crossing. Another characteristic feature that is ofinterest in
the root-locus method is the point where the root-locus crosses the imaginary axis
because the system stability changes at this point. If the imaginary axis crossing
is from right to left of the s-plane, the closed-loop becomes stable as the gain is
increased. Ifit is from left to right, then the closed-loop system becomes unstable
on increasing the gain.
The point(s) where the root-locus crosses the imaginar)r axis can be determined
by 1) using the Routh's criterion and finding the values of the gain k that give all
the zeros in any one row of the Routh's ta6ble-or 2) substituting s = jco in the
characteristic equation, setting both real and imaginary parts to zero and solving
for the gain k and frequency a>. We will illustrate this second procedure in the
following example.
Example 5.5 .
Sketch the root-locus for the unity feedback system with
G(s)=- k(s+4)
, s~s + )(s + 2)(s + 5)
Solution. We have four poles at s = 0, -1, -2, -5 and only one finite zero
at s - -4. Therefore, the other three missing zeros are at inftnity. We have four
branches of the root-locus. Furthermore, the root-locus will be symmetrical. with
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL3(50)