Feedback Control of Computing Systems

Chapter 9.1.1 - Steady-State Error with Integral Control

9.1.1   Steady-State Error with Integral Control

To show how the steady-state error of a system with integral control can be zero,
even with constant reference or disturbance inputs, we start with an example.

Example 9.1: Steady-state error of the IBM Lotus Domino Server with I control
Consider the IBM Lotus Domino Server with an integral controller. Its
control input is MaxUsers, and the output is RIS, the number of RPCs in
the Notes Server. The operating point of the IBM Lotus Domino Server is
. In our case, = (375, 325). The kth offset
value of the input is u(k) = MaxUsers(k) − , and for the output it
is y(k) = RIS(k) − . The block diagram is shown in Figure 9.1. As derived
in Example 3.7, the transfer function of the IBM Lotus Domino Server is

 

Referring to Figure 9.1, the closed-loop transfer function from the reference input
to the measured output is

 

Note that for any value of KI, the steady-state gain of this transfer function is 1:

 

From Equation (8.5), the steady-state error to a constant reference of magnitude
rss is

 

and thus, for any value of KI such that the closed-loop system is stable, the
steady-state error to a constant reference input is zero.

It turns out that the steady-state gain of a system with integral control does not
depend on the target system as long as the closed-loop system is stable. Indeed,
for a stable closed-loop system with integral control, the steady-state gain is 1.
This is a key result since having a steady-state gain of 1 means that there is no

  Fig. 9.1 Feedback loop with integral control.

steady-state error in response to step changes in the reference and disturbance
inputs.

The foregoing can be proved in a straightforward way. Referring to Figure 9.1,
we see that

 

Now observe that

 

Note that this result does not depend on KI as long as the closed-loop system is
stable.

Integral control also eliminates errors due to disturbance inputs. Consider again
the integral control system of Figure 9.1. The closed-loop transfer function for a
disturbance input is the forward gain from D(z) to Y(z) divided by 1 plus the
loop gain,

 

and the steady-state gain of this disturbance transfer function is

 

From Equation (8.6), the steady-state error to a constant disturbance of magnitude
dss is

 

Again, the steady-state error to a constant disturbance is zero for any value of
KI and for any system model G(z), such that the closed-loop system is stable.

In summary, integral control eliminates steady-state error due to step changes
in either the reference or disturbance inputs, as long as the closed-loop system
is stable.

 

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