The frequency-response techniques discussed in the previous chapters are the open-loop frequency plots that have obtained the information about the closed-loop stability using the open-loop frequency response of the system. In these methods, the frequency response of the loop transfer function is plotted and information regarding the closed-loop stability is derived from the plot. In this chapter, constant M-circles (magnitude), constant N-circles (phase) and Nichols chart are discussed, which directly give the information regarding the closed-loop stability of the system.
The closed-loop transfer function of a system with open-loop transfer function and feedback transfer function is
Substituting in the above equation, we obtain
Letting , we obtain
(10.1)
where is the magnitude of the closed-loop transfer function and is the phase angle of the closed-loop transfer function.
Since the magnitude and phase angle of the closed-loop system are the function of frequency , the closed-loop frequency plot of a system is the plot of magnitude and phase angle of the closed-loop system with respect to frequency . Analytically or graphically, the magnitude and phase angle of the closed-loop system for different values of can be calculated. In analytical method, tedious calculations are involved in determining the magnitude and phase angle of the closed-loop system for different values of . The graphical methods that eliminate the disadvantages of the analytical method are constant M- and N-circles and Nichols chart.
Let the open-loop transfer function of the system be . In frequency-response analysis, is replaced with . Therefore,
(10.2)
where is the real part of and is the imaginary part of .
The closed-loop transfer function of the system with unity feedback is obtained as
Substituting Eqn. (10.2) and using Eqn. (10.1) in the above equation, we obtain
The magnitude of the above equation is
Squaring both sides of the above equation and cross multiplying, we obtain
(10.3)
Simplifying the above equation, we get
i.e.,
Dividing the above equation by , we obtain
Adding the term on both sides of the above equation, we obtain
Upon simplifying, we obtain
i.e., , (10.4)
Equation (10.4) resembles the equation of a circle with centre and radius
The constant M-loci or constant M-circles are the family of circles described by Eqn. (10.4) in -plane when takes different values. The constant M-loci or constant M-circles for different values of are shown in Fig. 10.1.
The following three cases can be inferred from Fig. 10.1.
Fig. 10.1 ∣ Constant M-circles or constant M-loci
Case 1: M > 1
When the magnitude increases, the radius of -circles decreases and the centre of the -circles move towards the point . Therefore, when , the radius of -circle is zero and centre is at . This implies that the constant -circle at represents the point . These circles lie to the left of the circle.
Case 2: M = 1
When the magnitude is equal to 1, the radius of -circle is infinity and the centre of the -circle is . This implies that the constant -circles at represents a straight line parallel to imaginary axis and the intersection of the parallel line with the real axis can be determined by substituting in Eqn. (10.3). Thus, the intersection point of circle in the real axis is at .
Case 3: M < 1
When the magnitude decreases, the radius of -circles decreases and the centre of the -circles moves towards the origin. Therefore, when , the radius of -circles is zero and centre is at origin. This implies that the constant -circles at represents the origin.
The above three cases can be explained more clearly with the help of Table 10.1 which gives the centre and radius of -circles for different values of
Table 10.1 ∣ Centre and radius of M-circles
The polar plot of a loop transfer function and the constant M-circles for the same system are shown in Fig. 10.2.
Fig. 10.2 ∣ Polar plot and constant M-circles
The resonant peak and resonant frequency of the system are determined by using the following steps:
Step 1:The polar plot and constant M-circles for different values of M are drawn as shown in Fig. 10.2.
Step 2:The polar plot will intersect the constant M circles at more than one point.
Step 3:The frequency corresponding to the different intersection points is determined.
Step 4:The circles at which the polar plot is a tangent to the circle are determined and the corresponding M values are found.
Step 5:The value of M with smaller value is the resonant peak of the system.
Step 6:The frequency corresponding to the particular intersection point is the resonant frequency of the system .
For the polar plot and the constant M-circles shown in Fig. 10.2, the resonant peak is at and the resonant frequency is .
The flow chart for determining and from constant M-circles is shown in Fig. 10.3.
Fig. 10.3 ∣ Flow chart for determining Mr and ωr
The variation of gain K with the polar plot is shown in Fig. 10.4. It is evident that as the gain K increases, the values of resonant peak and resonant frequency will also increase.
Fig. 10.4 ∣ Polar plot and constant M-circles for different values of gain K
When the variation of magnitude of the system with respect to frequency alone is plotted as shown in Fig. 10.5, the bandwidth of the system can be calculated and this is depicted in Fig. 10.5.
Fig. 10.5 ∣ Magnitude versus curve
Also, the resonant peak and resonant frequency are also shown in Fig. 10.5.
The variation of resonant peak and resonant frequency with respect to variation in gain K is shown in Fig. 10.4. It is clear that, at gain , the resonant peak is . At this point, the system becomes marginally stable. Also, the system will be unstable when its gain is greater than .
The step-by-step procedure to determine the value of gain K corresponding to the desired resonant peak is given below:
Step 1:The polar plot of the system is drawn by assuming gain .
Step 2:The angle is determined by using the formula, .
Step 3:A radial line OA is drawn from the origin as shown in Fig. 10.6(a).
Step 4:The constant M-circle with with centre on the negative real axis is drawn, which is tangent to both the radial line OA and polar plot as shown in Fig. 10.6(a).
Step 5:Let the constant M-circle touch the radial line OA at B.
Step 6:A perpendicular line is drawn from the point B so that the line intersects the negative real axis at C.
Step 7:Thus, the desired gain K is obtained using the formula, .
Fig. 10.6(a) ∣ Gain K corresponding to
The flow chart for determining gain for desired resonant peak is given in Fig. 10.6(b).
Fig. 10.6(b) ∣ Flow chart for determining gain K for
The step-by-step procedure for determining the magnitude plot of the system using constant M-circles is given below:
Step 1:The polar plot of a system for the given gain is plotted in -plane.
Step 2:The constant M-circles for different values of M are plotted in the same -plane.
Step 3:The intersection points of the polar plot and constant M-circles are noted down.
Step 4:The frequency corresponding to an intersection point is noted down from polar plot and the magnitude corresponding to the intersection point is the value of M.
Step 5:Once the value of M and its corresponding frequency are noted down from the intersection points, the magnitude plot of the system is obtained by taking the value of M along Y-axis and corresponding frequency along X-axis.
The constant M-circles with polar plot of a system and its corresponding magnitude plot are shown in Figs. 10.7 and 10.8(a) respectively.
Fig. 10.7 ∣ Polar plot and constant M-circles
Fig. 10.8(a) ∣ Magnitude plot of the system
The flow chart for the determination of magnitude plot from constant M-circles is shown in Fig. 10.8(b).
Fig. 10.8(b) ∣ Flow chart for obtaining the magnitude plot from constant M-circles
Let the open-loop transfer function of the system be . In the frequency response analysis of the system s is replaced with . Therefore,
(10.5)
where u is the real part of and v is the imaginary part of .
The closed-loop transfer function of the system with unity feedback is obtained as
Substituting Eqn. (10.5) and using Eqn. (10.1) in the above equation, we obtain
The phase angle of the system is
Taking tan on both sides of the above equation, we obtain
Substituting in the above equation, we obtain
Using the formula in the above equation, we obtain
Simplifying the above equation, we obtain
Therefore,
Adding on both sides of the above equation, we obtain
Rearranging the above equation, we obtain
(10.6)
The above equation resembles the equation of a circle with centre and radius .
It is to be noted that irrespective of the value of N, Eqn. (10.6) gets satisfied for and . Therefore, each constant N-circle will pass through the origin and in the -plane.
The constant N-loci or constant N-circles are the family of circles described by Eqn. (10.6) in -plane when takes different values. The constant N-loci or constant N-circles for different values of are shown in Fig. 10.9.
The centre and radius of constant N-circles for different values of N are shown in Table 10.2.
Table 10.2 ∣ Centre and radius of N-circles
The constant N-circles shown in Fig. 10.9 for a given value of are only arc and not entire circles. Thus constant N-circles for Φ = 60° and Φ = 60° − 180° = −120° are parts of same circle.
Fig. 10.9 ∣ Constant N-circles or constant N loci
The step-by-step procedure for determining the phase plot of the system using constant N-circles is given below:
Step 1:The polar plot of a system for the given gain is plotted in -plane.
Step 2:The constant N-circles for different values of are plotted in the same -plane.
Step 3:The intersection points of the polar plot and constant N-circles are noted down.
Step 4:The frequency corresponding to an intersection point is noted down from polar plot and the magnitude corresponding to the intersection point is the value of .
Step 5:Once the value of and its corresponding frequency are noted down from the intersection points, the magnitude plot of the system is obtained by taking the value of along Y-axis and corresponding frequency along X-axis.
The phase plot for the system using constant N-circles is shown in Fig. 10.10(a).
Fig. 10.10(a) ∣ Phase angle plot of the system
The flow chart for determining the phase angle plot from constant N-circles is shown in Fig. 10.10(b).
Fig. 10.10(b) ∣ Flow chart for plotting phase angle plot of the system
The chart that results after the transformation of constant M- and N-circles to log-magnitude and phase angle coordinates is called Nichols chart. This transformation is first introduced by N.B. Nichols. In addition, the Nichols chart can be defined as the chart that consists of constant M- and N-circles superimposed on a graph sheet. The graph sheet consists of magnitude of the system in decibels which is obtained from constant M-circles along the Y-axis and phase angle of the system in degrees which is obtained from constant N-circles along the X-axis. The typical Nichols chart with constant M- and N-circles is shown in Fig. 10.11.
Fig. 10.11 ∣ Nichols chart
The reason for using Nichols chart for determining the stability of the system is due to the disadvantages that exist in working with the polar coordinates. The disadvantage is that when the loop gain of the system is changed, the polar plot will tend to change its shape. But in Bode plot or in magnitude versus phase plot, when the loop gain of the system is altered, the curve gets shifted up or down vertically. Therefore, it is convenient to work with Nichols chart compared to polar plot.
The advantages of Nichols chart are:
The transformation of constant M-circle into Nichols chart is explained using the step- by-step procedure as follows:
Step 1:The constant M-circles for M > 1 are plotted in Fig. 10.12(a).
Fig. 10.12(a) ∣ Constant M-circles of a system
Step 2:A line is drawn from the origin to any point on the constant M-circles as shown in Fig. 10.12(b).
Fig. 10.12(b) ∣ Line from origin to constant M-circles
Step 3:Consider a point A in the constant M-circles.
Step 4:The magnitude in dB and phase angle in degrees for that particular point are
Magnitude in dB =
Phase angle in degrees =
where is the length of the line OA and is the angle from the positive real axis to the line OA taken in the counterclockwise direction.
Step 5:Similarly, any point in the constant M-circles can be plotted in the Nichols chart.
Step 6:The constant M-circles shown in Fig. 10.12(a) are transformed to Nichols chart as shown in Fig. 10.12(c).
Fig. 10.12(c) ∣ Constant M circle in Nichols chart
It is noted that the critical point is plotted in Nichols chart as the point .
Similarly, the constant N-circles can be transformed into Nichols chart.
The different frequency domain specifications that can be determined by using Nichols chart are gain margin , phase margin , gain crossover frequency , phase crossover frequency and bandwidth .
The step-by-step procedure to determine the frequency domain specifications using Nichols chart is given below:
Step 1:Draw the plot in the Nichols chart.
Step 2:Transform the constant M-circles into the Nichols chart.
Step 3:Determine the value of at which the locus is a tangent to that particular M-circle.
Step 4:Determine the frequency of that particular point from plot.
Step 5:Then, the resonant peak and resonant frequency are determined as and .
Step 6:The gain crossover frequency and phase crossover frequency are the frequencies at which the plot crosses the 0dB line and −180° line in Nichols chart.
Step 7:Determine the gain margin and phase margin as shown in Fig. 10.13.
Step 8:The bandwidth of the system is determined as the frequency at which plot crosses the −3 dB or 0.707 circle.
Fig. 10.13 ∣ Determination of frequency domain specifications using Nichols chart
The gain K of the system can be determined for the desired value of frequency domain specifications. The step-by-step procedure for determining the gain K for the desired value of frequency domain specifications is discussed in this section.
Case 1: To determine the gain K for a desired gain margin
The step-by-step procedure to determine the gain K for is given below.
Step 1:Draw the plot for gain .
Step 2:Determine the magnitude in dB of for a phase angle of −180°.
Step 3:Determine the magnitude of in dB for which is given by .
Step 4:Determine .
Step 5:The plot will be shifted vertically upward or vertically downward based on the value of C.
If , the plot is shifted vertically upward by dB.
If , the plot is shifted vertically downward by dB.
If , the plot is neither shifted upward nor downward vertically.
Step 6:The gain K for is determined using the formula
The flow chart for determining the gain for is shown in Fig. 10.14(a).
Fig. 10.14(a) ∣ Flow chart for determining K for
Case 2: To determine the gain K for a desired phase margin
The step-by-step procedure to determine the gain K for is given below.
Step 1:Draw the plot for gain .
Step 2:Determine the angle of for as −180°.
Step 3:Determine the magnitude of in dB for degrees.
Step 4:The plot will be shifted vertically upward or vertically downward based on the value of E.
If , the plot is shifted vertically downward by dB.
If , the plot is shifted vertically upward by dB.
If , the plot is neither shifted upward nor downward vertically.
Step 6:The gain K for is determined by using the formula
The flow chart for determining the gain for is shown in Fig. 10.14(b).
Fig. 10.14(b) ∣ Flow chart for determining K for
Case 3: To determine the gain K for a desired resonant peak
The step-by-step procedure to determine the gain for is given below.
Step 1:Draw the plot for gain .
Step 2:Determine the resonant peak for the system .
Step 3:Trace the plot of with gain and move the plot either upward or downward based on so that the traced plot is a tangent to the contour.
Step 4:Determine the value F in dB by which the plot has moved.
Step 5:The gain K for is determined by using the formula,
The flow chart for determining the gain K for is shown in Fig. 10.14(c).
Fig. 10.14(c) ∣ Flow chart for determining K for
Case 4: To determine the gain K for a desired bandwidth
The step-by-step procedure to determine the gain K for is given below.
Step 1:Draw the plot for gain .
Step 2:Determine the magnitude of in dB for . Let it be dB.
Step 3:If the value of is equal to dB, then the plot is neither shifted vertically upward or downward. But, if the value of is not equal to dB, then the following steps are to be followed.
Step 4:Determine the point in the dB contour when it crosses dB.
Step 5:Trace the plot of with gain and move the plot either upward or downward so that it passes through the point .
Step 6:Determine the value in dB by which the plot has moved.
Step 7:The gain K for is determined by using the formula
The flow chart for determining the gain for is shown in Fig. 10.14(d).
Fig. 10.14(d) ∣ Flow chart for determining K for
Example 10.1: The loop transfer function of a system with a unity feedback is given by . Determine the gain margin, phase margin, gain crossover frequency, phase crossover frequency and bandwidth of the system using Nichols chart.
Solution:
The plot is plotted in the Nichols chart.
and
Table E10.1 ∣ Magnitude and phase angle of the system
Fig. E10.1 ∣ plot in Nichols chart
Gain margin, dB
Phase margin,
Gain crossover frequency, rad/s
Phase crossover frequency, rad/s
Example 10.2: The loop transfer function of an unity feedback system is . Using Nichols chart, determine the gain K so that (a) the desired gain margin of the system is 16 dB, (b) the desired phase margin of the system is 40° and (c) the desired resonant peak of the system is 5 dB.
Solution:
and
Table E10.2 ∣ Magnitude and phase angle of the system
Fig. E10.2(a)
Gain margin, dB
Phase margin, 59° and
Gain crossover frequency, rad/s
Case 1: When the desired gain margin of the system is 16 dB.
Fig. E10.2(b)
i.e., .
Case 2: When the phase margin of the system is 40°.
Fig. E10.2(c)
i.e., .
Case 3: When the desired resonant peak of the system, = 6 dB.
Fig. E10.2(d)
i.e., .
Thus, the frequency domain specifications for the system are determined and the gain values for the various desired frequency domain specifications are also determined.
Fig. Q10.14
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