1.2. Closed-Loop Control
The application of a negative feedback is not necessary to realize a control system. If there is enough a priori knowledge about the process then the open control loop can be used as shown in
Figure 1.2.1, where
P means the transfer function of the process and
C is the transfer function of the regulator. In the figure, the reference signal is
r,
y is the output signal (controlled signal),
u is the actuating signal, and
yni and
yno are the input and output noises, respectively. This scheme is called open-loop control.
The reference signal tracking would be ideal if the regulator could perform the inverse of the process transfer function, but the perfect inverse usually cannot be realized. The control can provide the reference signal tracking, but it cannot eliminate the effects of disturbances.
The control is performed via negative feedback, if the input signal (manipulated variable or actuating signal) of the process is influenced by the so-called error signal
e, which is the deviation between the measured and desired value of the process output signal. Based on the error signal
e, the regulator
C generates the manipulated variable
u, which modifies the output of the process
P. The output signal of the process changes according to the dynamics of the process until the output signal reaches its prescribed value. The negative feedback-based regulation is called closed-loop control. The block scheme of such a control system is given in
Figure 1.2.2. In many cases the reference signal is filtered via a term of transfer function
F (denoted by the dashed line in the figure).
Figure 1.2.1 The block scheme of open-loop control.
Figure 1.2.2 The block scheme of the closed-loop control system.
The relationships between the signals in
Figure 1.2.2 can be given by the following expressions:
(s)=F(s)C(s)P(s)1+C(s)P(s)R(s)+11+C(s)P(s)Yno(s)+P(s)1+C(s)P(s)Yni(s)
(s)=F(s)1+C(s)P(s)R(s)-11+C(s)P(s)Yno(s)-P(s)1+C(s)P(s)Yni(s)
(s)=F(s)C(s)1+C(s)P(s)R(s)-C(s)1+C(s)P(s)Yno(s)-C(s)P(s)1+C(s)P(s)Yni(s)
If
F(
s)=1, it is called the
one-
degree-
of-
freedom (
ODOF) control; if
F(
s) is a given transfer function, it is called the
TDOF control. In the case of
ODOF, four basic transfer functions and in the case of
TDOF, six basic transfer functions determine the signal transmissions between the output signals
y and
u, and the input signals: the reference signal and the output noise. Since the input noise
yni can always be transferred to an equivalent output disturbance
yn (see
Figure 1.2.3), so hereafter it is sufficient to investigate the following four transfer functions (the signs can be disregarded):
R=FCP1+CP;YYn=P1+CPUR=FC1+CP;YYn=11+CP
In the case of F=1 the transfer function of the system is
which is the complementary sensitivity function. Here L=CP is the so-called loop transfer function of the open-loop system. The error transfer function regarding the reference signal is
Figure 1.2.3 One-degree-of-freedom closed-loop control system.
and it is also called the sensitivity function. This terminology can be interpreted if the sensitivity of T is calculated for the change of the process.
Let us investigate the behavior of the control loop if the transfer function of the process changes from a nominal value P to ˆ=P+?P. This means, in addition, that instead of the ideal process only its model ˆ is known. Let the relative error of L be
that is, it is equal to the relative error of the process model. Then the relative error of T can be obtained by simple computation as
since
Thus the sensitivity function S shows how the relative change of the process influences the relative change of the overall transfer function. The complementary sensitivity function can be explained by the apparent relationship
The
TDOF control systems can also be given in the form shown in
Figure 1.2.4.
Figure 1.2.4 Two-degrees-of-freedom closed-loop control.
Figure 1.2.5 Equivalences of the two-degrees-of-freedom closed-loop controls.
M-a and E-ß Curves
For deeper analysis of the relationship between the frequency functions of the open- and closed-loop systems, let us analyze the following. The complementary sensitivity function of the closed system can be calculated by the expression
(1.2.5). The frequency function of the closed-loop system can be expressed by its amplitude and phase angle:
(j?)=L(j?)1+L(j?)=M(?)eja(?)
The gain of the closed system approaches the constant value one for high amplification value of the open system. This conclusion can be drawn from the expression
T(j?)|=|L(j?)L(j?)+1||L|»1˜1
Since the control, in general, ensures high gain in the low frequency region, the gain of the closed loop is close to one. Low gain values of the closed loop belongs to the low amplification values of the open loop
T(j?)|=|L(j?)L(j?)+1||L|«1˜|L(j?)|
Since the amplification of physical systems decreases at high frequencies, this expression can be interpreted as indicating that the amplification values of the open- and closed-loop systems are almost the same at high frequencies, that is, the negative feedback does not change the open loop.
During the control design, the relationship between the transfer functions of the closed loop T(s) and of the open loop L(s)=C(s)P(s) is taken into account. This relatively simple relationship actually means conform nonlinear mapping from a complex plane L(s) to T(s). This nonlinearity is the reason why the control design cannot always be performed unambiguously with simple methods.
Every mapping point (complex vector) can be determined for each point of the complex plane by the expression
(1.2.5). First, investigate what kinds of curves belong to the values
T|=M, where
M is a constant. The points of closed systems with the same amplitude correspond to circles on the complex plane. This can easily be verified by solving the equation
=|L(j?)1+L(j?)|=|u+jv1+u+jv|=u2+v21+2u+u2+v2
The equation of the curves belonging to the constant amplitude M can be obtained by rearranging the above equation as
This gives the equation of a circle with radius r and center point (uo,vo):
The curves belonging to different constant, closed-loop amplitudes
M are shown in
Figure 1.2.6.
The curve at M=1 is a vertical line at u=-0.5. For M>1, the curves are to the left of the line; for M<1, they are to the right of the line. If M tends to infinity, the curves shrink to the point...