Examine the effect of the open-loop gain K on stability and steady-state performance of the system shown in Fig. 14.8, which is subjected to unit ramp input signals.
Examine the effect of the open-loop gain K on stability and steady-state performance of the system shown in Fig. 14.8, which is subjected to unit ramp input signals.
The open-loop sinusoidal transfer function is
G_{(j\omega )} H_{(j\omega) } = T_{OL } (j\omega ) = \frac{K} {j\omega (j\omega +1) (j\omega +5)} .
The real and imaginary parts of T_{OL } (j\omega ) are
Re\left[ T_{OL } (j\omega )\right] =\frac{-6K}{(\omega ^{4}+26\omega ^{2}+25 )} ,
Im\left[ T_{OL } (j\omega )\right] =\frac{K(\omega ^{2}-5 )}{(\omega ^{5}+26\omega ^{3}+25\omega )} .
The stability gain margin k_{g} was defined in Chap. 13 as
K_{gdB} =20\log \frac{1}{\left|T_{OL } (j\omega _{p} )\right| } ,
where \omega _{P} is such that
\angle T_{OL } (j\omega _{P} )=-180° , or Im\left[ T_{OL } (j\omega )\right] =0 .
For this system \omega _{P} =\sqrt{5} rad/s, and the gain margin in decibels is
K_{gdB} =20\log \frac{30}{K } .
Now, to examine the steady-state performance of the system subjected to a unit ramp input u(t) = t, the static-velocity error coefficient must be determined. Using Equation (14.22) for a type 1 system yields
K_{V}=\underset{s\rightarrow 0}{\lim } \left[\frac{sK}{s(s+1)(s+5)} \right] =\frac{5}{K} ,
and hence the steady-state error is
e_{ss } =\frac{5}{K} .
Figure 14.9 shows the system gain margin k_{gdB} , static, velocity error coefficient K_{V} , and steady-state error e_{ss} as functions of the open-loop gain K. Note that the system is marginally stable for K= 30, at which the minimum steady-state error approaches 0.1667. Selecting values of K less than 30 will improve system stability at the cost of increasing steady-state error.