Chapter 6 · 6 hours
Frequency Response Techniques
IOE past exam questions
Past questions and answers
38 questions set from this chapter, 8 of them more than once. Most asked first.
- Asked 3 times
- 2082 Baisakh · 6+2+2 marks
- 2078 Kartik · 8 marks
- 2070 Chaitra · 8 marks
Construct complete Nyquist plot for a unity feedback control system whose open loop transfer function is G(s) = (s+2)/(s²−1). Check stability of the system as per Nyquist Criterion. What is its gain margin?
Answer
The open-loop poles are and , so P = 1 (one RHP pole). No poles lie on the -axis, so the Nyquist contour needs no indentation.
Frequency response
| ω | Re | Im | |G| | ∠G |
|---|---|---|---|---|
| 0 | −2 | 0 | 2 | −180° |
| 0.5 | −1.60 | −0.40 | 1.65 | −166° |
| 1 | −1.00 | −0.50 | 1.12 | −153.4° |
| 2 | −0.40 | −0.40 | 0.57 | −135° |
| 5 | −0.08 | −0.19 | 0.21 | −111.8° |
| ∞ | 0 | 0 | 0 | −90° |
- For the imaginary part is always negative, so the plot lies in the third quadrant. It runs from (at ω = 0) to the origin (at ω = ∞), arriving along .
- The part for is the mirror image about the real axis.
- The large semicircle (, ) maps to the origin, because .
Complete Nyquist plot
|
|
|
|
................ |
...... ...... |
.... ....|
.. ..
--------*---------------@----------------*--------
** **
**** ****|
****** ****** |
**************** |
|
|
|
|
-2 -1 0
* w > 0 . w < 0 (mirror) @ point (-1, j0)
w = 0 at -2; w -> +-inf at origin
Stability by Nyquist criterion
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
- As ω goes from to , the plot runs from the origin through the upper half to , then through the lower half back to the origin. This is a closed curve traced counter-clockwise.
- The point lies inside it, since the plot crosses the real axis at , to the left of .
- So (one counter-clockwise encirclement).
The closed-loop system is stable. Check: , whose roots are in the LHP. ✓
Gain margin
The plot cuts the negative real axis at ω = 0 (phase crossover frequency ), where .
Because the open loop is unstable, a negative GM does not mean instability here. It means the loop gain can be reduced by a factor of 2 before the system becomes unstable. (With gain : is stable only for .)
Answer: P = 1, N = −1 (one CCW encirclement), Z = 0, so the closed loop is stable. GM = 0.5 (−6.02 dB).
- Asked 3 times
- 2080 Bhadra · 8 marks
- 2068 Baisakh (old course) · 8 marks
- 2078 Kartik · 8 marks
Sketch an approximate polar plot for a unity feedback system with a feedforward transfer function: G(s) = 10/[s(s+1)²]. And obtain (i) GM (ii) PM (iii) gcf (iv) pcf and (v) Stability.
Answer
Key points of the polar plot
| ω | |G| | ∠G | Re | Im |
|---|---|---|---|---|
| 0⁺ | ∞ | −90° | −20 (asymptote) | −∞ |
| 0.2 | 48.1 | −112.6° | −18.5 | −44.4 |
| 0.5 | 16.0 | −143.1° | −12.8 | −9.6 |
| 1 | 5.0 | −180° | −5.0 | 0 |
| 2 | 1.0 | −216.9° | −0.8 | 0.6 |
| 5 | 0.077 | −247.4° | −0.03 | 0.07 |
| ∞ | 0 | −270° | 0 | 0 |
- Low-frequency asymptote: . The plot starts at along the line Re = −20.
- Real-axis crossing: , where . The plot cuts the negative real axis at −5.
- High frequency: the plot reaches the origin along (from the second quadrant, tangent to the +j axis).
. |
.. |
... |
.. |
... |
... |
... |
.... **** |
-------------------------------*******--@**-------
**** .... |
*** |
*** |
*** |
** |
*** |
** |
* |
-20 -5 0
* w > 0 . w < 0 (mirror) @ point (-1, j0)
crosses real axis at -5 (w = 1); asymptote Re = -20
(iv) Phase crossover frequency (pcf)
rad/s.
(i) Gain margin
(iii) Gain crossover frequency (gcf)
(Check: .)
(ii) Phase margin
(v) Stability
GM < 0 dB and PM < 0. The polar plot crosses the real axis at −5, to the left of −1, so the point is enclosed. With P = 0, the complete Nyquist plot encircles −1 twice clockwise, so Z = 2. The closed-loop system is unstable, with two RHP poles.
Check with Routh: gives , so it is unstable. For stability must be below 2, i.e. the gain must be reduced by a factor of 5.
Answer: GM = −13.98 dB, PM = −36.87°, gcf = 2 rad/s, pcf = 1 rad/s. The system is unstable.
- Asked 3 times
- 2079 Bhadra · 8+2 marks
- 2067 Asar (old course) · 8 marks
- 2080 Bhadra · 6+2 marks
Using Nyquist criteria, determine the stability of the closed loop system whose open loop transfer function is given by G(s)H(s) = 50/[(s+1)(s+2)]; also find the phase margin.
Answer
Open-loop poles
and , so P = 0. There are no poles on the -axis.
Polar (ω: 0 → ∞) data
| ω | |G| | ∠G | Re | Im |
|---|---|---|---|---|
| 0 | 25 | 0° | 25 | 0 |
| 1 | 15.81 | −71.6° | 5.0 | −15.0 |
| 2 | 7.91 | −108.4° | −2.5 | −7.5 |
| 5 | 1.82 | −146.9° | −1.53 | −0.99 |
| 6.89 | 1.00 | −155.6° | −0.91 | −0.41 |
| 10 | 0.49 | −163.0° | −0.47 | −0.14 |
| ∞ | 0 | −180° | 0 | 0 |
- The plot starts at 25 on the positive real axis, goes through the 4th and 3rd quadrants, and reaches the origin along .
- The phase reaches only at ω = ∞, so the plot never cuts the negative real axis at a finite point.
- The part is its mirror image. The infinite semicircle of the s-plane maps to the origin.
| ................
| ...... .......
.... ....
...| ....
.. | ..
.. | ...
.. | ..
.. | .
-----*@**-------------------------------------*---
** | *
** | **
** | ***
** | **
***| ****
**** ****
| ****** *******
| ****************
0 25
* w > 0 . w < 0 (mirror) @ point (-1, j0)
w = 0 at 25; ends at origin along -180 deg
Nyquist stability
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
The closed curve passes between the origin and the far right (25). The point lies outside the curve, so .
The closed-loop system is stable for this gain (and in fact for any , because the plot never crosses the negative real axis, so GM = ∞).
Phase margin
Gain crossover: :
Answer: N = 0, P = 0, so Z = 0 and the closed loop is stable. PM ≈ 24.4° at = 6.89 rad/s (GM = ∞).
- Asked 3 times
- 2078 Bhadra · 6+2 marks
- 2075 Chaitra · 10 marks
- 2081 Bhadra · 6+2+2 marks
A unity feedback system has open loop transfer function G(s) = 1/[s(1+2s)(1+s)]. Sketch Nyquist plot for the system and therefore obtain the gain margin. Check stability by Nyquist criterion.
Answer
Nyquist contour
There is a pole at the origin, so the contour is indented around it by a small semicircle with θ from −90° to +90°. Open-loop poles in the RHP: P = 0.
Mapping of each section
- ω = 0⁺ to ∞ (positive -axis):
| ω | |G| | ∠G | Re | Im |
|---|---|---|---|---|
| 0.1 | 9.76 | −107.0° | −2.86 | −9.33 |
| 0.3 | 2.74 | −137.7° | −2.02 | −1.84 |
| 0.5 | 1.26 | −161.6° | −1.20 | −0.40 |
| 0.707 | 0.667 | −180° | −0.667 | 0 |
| 1 | 0.316 | −198.4° | −0.30 | 0.10 |
| ∞ | 0 | −270° | 0 | 0 |
- Low-frequency asymptote: . The plot starts at along Re = −3.
- Phase crossover: rad/s.
- , so it crosses at −0.667.
- ω = −∞ to 0⁻: mirror image of the above.
- Infinite semicircle: , so it maps to the origin.
- Small semicircle at origin: . As θ goes from −90° to +90°, sweeps an infinite-radius arc clockwise from +90° through 0° to −90° (right half of the G-plane), joining the ω = 0⁻ end to the ω = 0⁺ end.
.. |
.. |
.. |
.. |
... |
.. |
.... |
..... |
-----------------------------@**********----------
***** |
**** |
** |
*** |
** |
** |
** |
** |
-3 -0.67 0
* w > 0 . w < 0 (mirror) @ point (-1, j0)
crosses at -0.667 (w = 0.707); asymptote Re = -3
(The infinite clockwise arc on the right closes the curve.)
Gain margin
The phase margin (for reference) is at rad/s.
Stability by Nyquist criterion
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
The plot crosses the negative real axis at −0.667, to the right of −1, so the point is not encircled: N = 0.
The closed-loop system is stable. Check: has Routh first column , all positive. ✓
Answer: GM = 1.5 (3.52 dB) at = 0.707 rad/s. N = 0, P = 0, Z = 0, so the system is stable.
- Asked 2 times
- 2078 Kartik · 3 marks
- 2068 Chaitra · 6 marks
Find the open loop transfer function with the help of following Bode plot. [Figure: asymptotic magnitude plot; 20 dB at ω = 0.1, falling at −20 dB/dec through 0 dB at ω = 1, then changing at ω = 2 to −40 dB/dec (axis marks at 0.1, 1, 2, 5, 10)]
Answer
A Bode magnitude asymptote is read segment by segment. The initial slope gives the type and gain, and each change of slope gives a corner frequency.
Reading the plot
- Initial slope −20 dB/dec: one pole at the origin (type 1), i.e. a factor .
- Gain K: the −20 dB/dec line (or its extension) cuts 0 dB at . It crosses 0 dB at ω = 1, so K = 1. Check at ω = 0.1: dB, which matches the plot.
- At ω = 2 the slope changes from −20 to −40 dB/dec: the change is −20 dB/dec, so there is a simple pole with corner frequency 2 rad/s, i.e. a factor .
- There are no further changes, so there are no more poles or zeros.
Transfer function
Check
| ω | Asymptote (−20 line) | Plot |
|---|---|---|
| 0.1 | 20 dB | 20 dB ✓ |
| 1 | 0 dB | 0 dB ✓ |
| 2 | −6.02 dB | corner ✓ |
| 10 | dB | on −40 line ✓ |
Answer: , i.e. .
- Asked 2 times
- 2076 Chaitra · 5+1+2 marks
- 2074 Chaitra · 8 marks
Sketch the Nyquist contour and plot of unity feedback system having open loop transfer function G(s)H(s) = (s+10)/[(s−3)(s+3)]. (i) Comment on stability. (ii) Determine gain margin.
Answer
Open-loop poles: and , so P = 1.
Nyquist contour
The contour encloses the whole right half of the s-plane:
- the -axis from to ;
- a semicircle of infinite radius on the right, traversed clockwise.
No poles lie on the -axis, so no indentation is needed. The RHP pole at lies inside the contour.
jw
^ +j inf
|\
| \ R -> inf
| \
------+---x----> σ
| / +3 (inside)
| /
|/
-j inf
Mapping
| ω | Re | Im | ∠G |
|---|---|---|---|
| 0 | −1.111 | 0 | −180° |
| 1 | −1.000 | −0.100 | −174.3° |
| 3 | −0.556 | −0.167 | −163.3° |
| 5 | −0.294 | −0.147 | −153.4° |
| 10 | −0.092 | −0.092 | −135° |
| ∞ | 0 | 0 | −90° |
- For ω > 0 the plot lies in the third quadrant, from to the origin.
- The ω < 0 part is the mirror image.
- The infinite arc maps to the origin.
|
|
|
|
|
|
....................... |
..... ....|
-----------*--@-------------------------**--------
***** ****|
*********************** |
|
|
|
|
|
|
-1.11 0
* w > 0 . w < 0 (mirror) @ point (-1, j0)
w = 0 at -1.111; w -> +-inf at origin
(i) Stability
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
As ω goes from −∞ to +∞, the closed curve runs from the origin through the upper half to , then through the lower half back to the origin. This is counter-clockwise, and lies inside because . So N = −1.
The closed-loop system is stable. Check: , with roots in the LHP. ✓
(ii) Gain margin
Phase crossover is at ω = 0, where .
Since the open loop is unstable, this means the gain may be reduced only by a factor of 0.9 before instability. With a gain , stability needs .
Answer: P = 1, N = −1, Z = 0, so the system is stable. GM = 0.9 (−0.92 dB).
- Asked 2 times
- 2074 Asoj · 8 marks
- 2079 Bhadra · 8 marks
The open loop transfer function of a control system is G(s)H(s) = (4s+1)/[s²(s+1)(2s+1)]. Using Nyquist criterion, determine the open loop and closed loop stability of this system.
Answer
Open-loop stability
Open-loop poles: . None lie in the RHP, so P = 0. However, the double pole at the origin makes the open-loop system itself not stable: its impulse response contains a term that grows without bound. In Nyquist terms we take P = 0 and indent the contour around the origin.
Mapping the Nyquist contour
| ω | |G| | ∠G | Re | Im |
|---|---|---|---|---|
| 0.1 | 105.1 | −175.2° | −104.7 | −8.76 |
| 0.2 | 29.1 | −174.5° | −29.0 | −2.82 |
| 0.354 | 10.66 | −180° | −10.66 | 0 |
| 0.5 | 5.66 | −188.1° | −5.60 | +0.80 |
| 1 | 1.30 | −212.5° | −1.10 | +0.70 |
| 2 | 0.22 | −236.5° | −0.12 | +0.18 |
| ∞ | 0 | −270° | 0 | 0 |
- ω = 0⁺ → ∞: the plot starts at infinity just below the negative real axis (angle slightly above −180°). It cuts the negative real axis where
So the crossing is at −10.67. The plot then enters the second quadrant and reaches the origin along −270°. 2. ω = −∞ → 0⁻: the mirror image. 3. Infinite semicircle: maps to the origin. 4. Small semicircle around the double pole: . As θ goes from −90° to +90°, traces a full 360° clockwise circle of infinite radius, from +180° through 0° to −180°.
|
|
|
|
|
*************** |
... ******** **** |
....... ******* **|
--------*******---------------------------@--**---
******* ....... ..|
*** ........ .... |
............... |
|
|
|
|
|
-10.67 0
* w > 0 . w < 0 (mirror) @ point (-1, j0)
crosses at -10.67 (w = 0.354)
(An infinite clockwise circle joins the ω = 0⁻ and ω = 0⁺ ends.)
Closed-loop stability
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
The point −1 lies between the crossing at −10.67 and the origin. Following the plot together with the infinite 360° clockwise arc, the point (−1, j0) is encircled twice clockwise: N = 2.
The closed-loop system is unstable, with 2 poles in the RHP.
Check (Routh):
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 2 | 1 | 1 | |
| 3 | 4 | ||
| −1.667 | 1 | ||
| 5.8 | |||
| 1 |
There are two sign changes, so there are 2 RHP poles (they are at ). ✓
Answer: Open loop: no RHP poles (P = 0), but the repeated pole at the origin makes it unstable in the BIBO sense. Closed loop: N = 2, Z = 2, so it is unstable.
- Asked 2 times
- 2070 Chaitra (old course) · 10 marks
- 2065 Shrawan (old course) · 8 marks
Draw the Nyquist plot for the following open loop transfer function G(s)H(s) = (s+2)/[s(s+1)(s+3)].
Answer
Open-loop poles: , so P = 0. There is one pole at the origin, so the contour is indented there.
1. Magnitude and phase
2. Real and imaginary parts
- Im < 0 for every ω > 0, so the plot never crosses the real axis at a finite frequency. The phase approaches −180° only as ω → ∞.
- Low-frequency asymptote: as ω → 0, Re → . (Equivalently .)
3. Table (ω > 0)
| ω | |G| | ∠G | Re | Im |
|---|---|---|---|---|
| 0⁺ | ∞ | −90° | −0.556 | −∞ |
| 0.1 | 6.64 | −94.8° | −0.55 | −6.62 |
| 0.5 | 1.21 | −112.0° | −0.45 | −1.12 |
| 1 | 0.50 | −126.9° | −0.30 | −0.40 |
| 2 | 0.175 | −142.1° | −0.14 | −0.11 |
| 5 | 0.036 | −159.5° | −0.03 | −0.01 |
| ∞ | 0 | −180° | 0 | 0 |
4. Mapping of the full contour
- ω = 0⁺ → +∞: from (along Re = −0.556) down to the origin, arriving at −180° (third quadrant).
- ω = −∞ → 0⁻: mirror image in the second quadrant.
- Infinite semicircle: maps to the origin.
- Small indentation at s = 0: maps to an infinite arc, clockwise through the right half-plane (from +90° to −90°).
.. |
. |
.. |
.. |
.. |
... |
... |
..... |
-------@---------------------------*****----------
***** |
*** |
*** |
** |
** |
** |
* |
** |
-0.556 0
* w > 0 . w < 0 (mirror) @ point (-1, j0)
asymptote Re = -0.556; no negative real crossing
5. Stability
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
The plot never cuts the negative real axis, so is not encircled: N = 0, and .
The closed-loop system is stable. Also, GM = ∞ and PM = 64.8° (at = 0.588 rad/s).
Check: gives Routh first column , all positive. ✓
- 2081 Bhadra · 8 marks
Draw bode plot for open loop transfer function of closed loop system as G(s) = 512(s+3)/[s(s²+16s+256)]. Also comment on stability.
Answer
Time-constant form
Quadratic factor: rad/s and , so .
Factors and corner frequencies
| Factor | Corner (rad/s) | Slope change | Phase |
|---|---|---|---|
| — | dB | 0° | |
| — | −20 dB/dec | −90° | |
| 3 | +20 dB/dec | ||
| quadratic, ζ = 0.5 | 16 | −40 dB/dec | 0 to −180° |
Magnitude asymptotes
| Range | Slope | Value |
|---|---|---|
| ω < 3 | −20 dB/dec | 35.56 dB at 0.1; 15.56 dB at 1; 6.02 dB at 3 |
| 3 < ω < 16 | 0 dB/dec | 6.02 dB |
| ω > 16 | −40 dB/dec | 0 dB at ; −25.8 dB at 100 |
With ζ = 0.5 the resonant correction at is dB, so the asymptotes are close to the true curve.
Phase
| ω | 0.1 | 1 | 3 | 5 | 10 | 16 | 24.4 | 50 | 100 | ∞ |
|---|---|---|---|---|---|---|---|---|---|---|
| φ (deg) | −88.5 | −75.2 | −56.0 | −50.1 | −62.4 | −100.6 | −137.9 | −163.8 | −172.4 | −180 |
Bode plot
40 |*
|*******
| ******
10 | **************
|-------------------------****-----------------
| ****
-20 | ***
| ***
| ****
-50 | ****
| ****
| *
-80 |
+----------------------------------------------
0.1 1 10 100 1000
Magnitude asymptotes (dB) vs w (rad/s)
0 |
|
|
-45 | ****
| ***** ***
| ******* **
-90 |********* **
| *
| **
-135 | **
| ***
| ******
-180 |----------------------------------************
+----------------------------------------------
0.1 1 10 100 1000
Phase (deg); -180 line shown
Margins and stability
- Gain crossover: the exact at rad/s (asymptotic estimate 22.6 rad/s). There, φ = −137.9°, so
- Phase crossover: the phase tends to −180° only as ω → ∞, so it never actually crosses −180°. Hence and GM = ∞.
Both margins are positive, so the closed-loop system is stable, with PM ≈ 42° (reasonably damped). Check: gives . ✓
Answer: GM = ∞, PM ≈ 42.1° (at 24.4 rad/s). The system is stable.
- 2081 Bhadra · 8+2 marks
Construct complete Nyquist plot for a unity feedback control system whose open loop transfer function is: G(s) = K/[s(s²+2s+2)]. Find maximum value of K for which the system is stable as per Nyquist Criterion.
Answer
Poles: . P = 0. The pole at the origin needs an indentation.
Frequency response
| ω | |G|/K | ∠G | Re/K | Im/K |
|---|---|---|---|---|
| 0⁺ | ∞ | −90° | −0.5 | −∞ |
| 0.5 | 0.99 | −119.7° | −0.49 | −0.86 |
| 1 | 0.447 | −153.4° | −0.40 | −0.20 |
| 1.414 | 0.25 | −180° | −0.25 | 0 |
| 2 | 0.112 | −206.6° | −0.10 | +0.05 |
| ∞ | 0 | −270° | 0 | 0 |
- Low-frequency asymptote: Re → −K/2.
- Real-axis crossing: Im = 0 when , so rad/s, where . The crossing is at −K/4.
- High frequency: reaches the origin along −270° (from the second quadrant).
Complete Nyquist plot
- ω = 0⁺ → ∞: from (along Re = −K/2), crossing at −K/4, to the origin.
- ω = −∞ → 0⁻: mirror image.
- Infinite semicircle: maps to the origin.
- Indentation at s = 0: maps to an infinite arc clockwise from +90° through 0° to −90°.
. |
. |
. |
. |
.. |
.. |
... |
... |
----@------------------------*************--------
*** |
*** |
** |
** |
* |
* |
* |
* |
-1 -0.5 -.25
* w > 0 . w < 0 (mirror) @ point (-1, j0)
drawn for K = 1: crosses at -0.25 (w = 1.414);
asymptote Re = -0.5. For gain K, scale every point by K.
Maximum K for stability
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
With P = 0, stability needs N = 0, i.e. the point −1 must lie to the left of the crossing:
If the crossing moves left of −1, giving N = 2 and Z = 2 (unstable). At the plot passes through −1: marginal stability with oscillation at rad/s.
Check (Routh): is stable if , i.e. . ✓
Answer: K_max = 4. The system is stable for 0 < K < 4 and oscillates at 1.414 rad/s when K = 4.
- 2081 Baisakh · 8 marks
Draw the Nyquist plot for the open loop transfer function given below and comment on closed loop stability. G(s) = 2.2/[s(s+1)(s²+2s+2)]
Answer
Poles: , so P = 0. The pole at the origin is indented.
Frequency response
| ω | |G| | ∠G | Re | Im |
|---|---|---|---|---|
| 0⁺ | ∞ | −90° | −2.2 | −∞ |
| 0.1 | 10.95 | −101.5° | −2.17 | −10.73 |
| 0.3 | 3.51 | −124.1° | −1.97 | −2.90 |
| 0.5 | 1.95 | −146.3° | −1.62 | −1.08 |
| 0.816 | 0.990 | −180° | −0.990 | 0 |
| 1 | 0.696 | −198.4° | −0.66 | +0.22 |
| 2 | 0.110 | −270° | 0 | +0.11 |
| ∞ | 0 | −360° | 0 | 0 |
- Low-frequency asymptote: , so Re → .
- Phase crossover: at has imaginary part , so rad/s. The real part is , so .
- The plot cuts the negative real axis at −0.99, then passes through the second quadrant (crossing the +j axis at ω = 2, where ∠G = −270°) and reaches the origin along −360°.
.. |
. |
.. |
.. |
.. |
... |
... |
..... **********|
--------------------------**@****--------**-------
***** ..........|
*** |
*** |
** |
** |
** |
* |
** |
-2.2 -0.99 0
* w > 0 . w < 0 (mirror) @ point (-1, j0)
crosses at -0.99 (w = 0.816), just right of -1
Stability
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
The crossing at −0.99 lies just to the right of −1, so the point is not encircled: N = 0 and .
The closed-loop system is stable, but only barely:
The closed-loop poles are at and . The dominant pair is almost on the -axis, so the step response will be a very lightly damped oscillation at about 0.81 rad/s. The gain limit (Routh) is , so a 1% gain increase would make the system unstable.
Answer: N = 0, Z = 0, so the system is stable (marginally: GM ≈ 0.09 dB, PM ≈ 0.5°).
- 2080 Baisakh · 10 marks
Draw Bode plot for given open loop transfer function G(s)H(s) = 50(s+10)/[(s+1)(s+100)]. Also comment on stability from the plot.
Answer
Time-constant form
It is a type-0 system with , so dB.
Corner frequencies
| Factor | Corner (rad/s) | Slope change |
|---|---|---|
| 1 | −20 dB/dec | |
| 10 | +20 dB/dec | |
| 100 | −20 dB/dec |
Magnitude asymptotes
| Range | Slope | Value at ends |
|---|---|---|
| ω < 1 | 0 | 13.98 dB |
| 1 – 10 | −20 dB/dec | 13.98 → −6.02 dB |
| 10 – 100 | 0 | −6.02 dB |
| ω > 100 | −20 dB/dec | −26.02 dB at 1000 |
The asymptotic gain crossover is where , i.e. ω = 5 rad/s. The exact value is 5.64 rad/s.
Phase
| ω | 0.1 | 1 | 2 | 5 | 5.64 | 10 | 20 | 50 | 100 | 1000 |
|---|---|---|---|---|---|---|---|---|---|---|
| φ (deg) | −5.2 | −39.9 | −53.3 | −55.0 | −53.7 | −45.0 | −35.0 | −36.7 | −50.1 | −84.8 |
The phase dips to about −55° near ω ≈ 4 and tends to −90° at high frequency. It never reaches −180°.
Bode plot
15 |*************
| ****
| ****
0 |------------------***-------------------------
| ***************
| ***
-15 | ****
| ****
| ***
-30 |
|
|
-45 |
+----------------------------------------------
0.1 1 10 100 1000
Magnitude asymptotes (dB) vs w (rad/s)
0 |***
| ******
| **** *******
-45 | **** ****** ****
| ******* ****
| ******
-90 | ***
|
|
-135 |
|
|
-180 |----------------------------------------------
+----------------------------------------------
0.1 1 10 100 1000
Phase (deg); never reaches -180
Stability from the plot
- Phase margin: at rad/s, φ = −53.7°, so .
- Gain margin: the phase never crosses −180°, so and GM = ∞.
Both margins are positive and large, so the closed-loop system is stable (and stays stable for any increase in gain). Check: the closed loop has both roots in the LHP. ✓
Answer: PM ≈ 126°, GM = ∞. The system is stable.
- 2080 Baisakh · 8 marks
What is Nyquist Contour? Map the Nyquist contour of open loop transfer function G(s) = 200/[(s+3)(s+1)(s+2)] into G(s) plane and apply Nyquist criterion to check the stability of closed loop system.
Answer
Nyquist contour
The Nyquist contour is a closed path in the s-plane that encloses the entire right half-plane. It consists of:
- the whole -axis from to ;
- a semicircle of infinite radius (, , θ from +90° to −90°), traversed clockwise;
- small semicircular indentations (radius ε → 0) around any open-loop poles that lie on the -axis, so the path avoids them.
Mapping this contour through gives the Nyquist plot. By the argument principle, the encirclements of count the RHP zeros of , i.e. the RHP closed-loop poles.
Mapping
Open-loop poles: , so P = 0. No indentation is needed.
| Section | Mapping |
|---|---|
| ω = 0 | |
| ω = 1 | (crosses the −j axis) |
| ω = 2 | |
| ω = √11 = 3.317 | Im of denominator = 0, Re = , so |
| ω = 5 | (second quadrant) |
| ω → +∞ | |
| ω < 0 | mirror image about the real axis |
| infinite semicircle | maps to the origin |
|........................
..... ......
... | ....
... | ...
.. | ...
. | ..
.. | ..
.. | .
---*****@*-------------------------------------*--
** | *
** | **
* | **
** | ***
*** | ***
*** | ****
***** ******
|************************
-3.33 33.3
* w > 0 . w < 0 (mirror) @ point (-1, j0)
w = 0 at 33.3; crosses at -3.33 (w = 3.317)
Nyquist criterion
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
The plot crosses the negative real axis at −3.33, to the left of −1. The closed curve (ω from −∞ to +∞) goes round the point twice clockwise, so N = 2.
The closed-loop system is unstable, with two closed-loop poles in the RHP.
- Gain margin: dB (negative).
- The gain would have to be reduced below for stability.
- Check (Routh): gives , so it is unstable. ✓
- 2079 Bhadra · 8 marks
Draw Bode plot for system with open loop transfer function G(s)H(s) = 60/[s(s+2)(s+6)]. Also find GM and comment on stability.
Answer
Time-constant form
( dB), type 1. Corner frequencies: 2 and 6 rad/s.
Magnitude asymptotes
| Range | Slope | Values |
|---|---|---|
| ω < 2 | −20 dB/dec | 33.98 dB at 0.1; 13.98 dB at 1; 7.96 dB at 2 |
| 2 – 6 | −40 dB/dec | 7.96 → dB |
| ω > 6 | −60 dB/dec | −24.4 dB at 10; −42.5 dB at 20 |
Phase
| ω | 0.1 | 0.5 | 1 | 2 | 2.71 | 3.46 | 4 | 6 | 10 | 20 |
|---|---|---|---|---|---|---|---|---|---|---|
| φ (deg) | −93.8 | −108.8 | −126.0 | −153.4 | −167.8 | −180.0 | −187.1 | −206.6 | −227.7 | −247.6 |
Bode plot
40 |
|********
| ********
10 | ********
|---------------------****---------------------
| ****
-20 | ***
| ****
| ***
-50 | ****
| ***
| ****
-80 | ***
+----------------------------------------------
0.1 1 10 100
Magnitude asymptotes (dB) vs w (rad/s)
-90 |*****
| *********
| ****
-135 | ****
| ***
| ***
-180 |----------------------***---------------------
| ***
| ***
-225 | ****
| ****
| ********
-270 | ****
+----------------------------------------------
0.1 1 10 100
Phase (deg); crosses -180 at 3.46 rad/s
Gain margin
Phase crossover:
(The asymptotic plot gives about −1.6 dB at 3.46 rad/s, i.e. GM ≈ 1.6 dB; the exact value is 4.08 dB.)
Phase margin
Exact gain crossover: rad/s, where φ = −167.8°, so .
Stability
GM = +4.08 dB > 0 and PM = +12.2° > 0, and . The closed-loop system is stable, but with small margins, so the response will be quite oscillatory.
Check: gives . ✓ The gain could rise by a factor of 1.6 (to 96) before instability.
Answer: GM = 4.08 dB at = 3.46 rad/s. PM ≈ 12.2°. The system is stable.
- 2076 Chaitra · 10 marks
Draw Bode plot for unity feedback system with open loop transfer function G(s) = 40(s+2)/[(2 + s + 25s²)(1+2s)s]. Find GM and comment on stability.
Answer
Time-constant form
Quadratic factor: , so rad/s; , so (very lightly damped).
Factors
| Factor | Corner (rad/s) | Slope change | Phase |
|---|---|---|---|
| — | 32.04 dB | 0° | |
| — | −20 dB/dec | −90° | |
| quadratic, ζ = 0.071 | 0.283 | −40 dB/dec | 0 to −180° (sharp) |
| 0.5 | −20 dB/dec | 0 to −90° | |
| 2 | +20 dB/dec | 0 to +90° |
Magnitude asymptotes
| Range | Slope | Values |
|---|---|---|
| ω < 0.283 | −20 dB/dec | 72.0 dB at 0.01; 52.0 dB at 0.1; 43.0 dB at 0.283 |
| 0.283 – 0.5 | −60 dB/dec | 43.0 → 28.2 dB |
| 0.5 – 2 | −80 dB/dec | 28.2 → −20.0 dB |
| ω > 2 | −60 dB/dec | −61.9 dB at 10 |
Resonant correction at : dB, so the true peak is about 59 dB near 0.28 rad/s.
Phase
| ω | 0.01 | 0.1 | 0.2 | 0.25 | 0.275 | 0.283 | 0.3 | 0.5 | 1 | 2 | 10 |
|---|---|---|---|---|---|---|---|---|---|---|---|
| φ (deg) | −91 | −102 | −117 | −139 | −180 | −201 | −242 | −294 | −304 | −300 | −278 |
Bode plot
90 |
|****
| *************
45 | *********
| *****
| ***
0 |-----------------------------****-------------
| ****
| *****
-45 | *****
| ***
|
-90 |
+----------------------------------------------
0.01 0.1 1 10
Magnitude asymptotes (dB); true peak ~59 dB at 0.28
-90 |***************
| *******
| **
-150 | *
|---------------------*------------------------
| *
-210 | *
| *
| *
-270 | * **
| ***** **********
| ********
-330 |
+----------------------------------------------
0.01 0.1 1 10
Phase (deg); crosses -180 at 0.275 rad/s
Gain margin
The phase crosses −180° at rad/s, just below . Because of the resonance, the magnitude there is very large: (58.8 dB).
Phase margin
Gain crossover is at rad/s (asymptotic estimate 1.12), where φ = −304.5°.
Stability
GM is negative (in dB), PM is negative, and . The closed-loop system is unstable.
Check: gives Routh first column . There are two sign changes, so there are 2 RHP poles. ✓
Answer: GM ≈ −58.8 dB, PM ≈ −124.5°. The system is unstable.
- 2076 Asoj · 8 marks
The open loop transfer function of closed loop system is G(s) = 2/[s(s+1)(2s+1)]. Using Nyquist Criterion, determine closed loop stability of this system.
Answer
Open-loop poles: , so P = 0. The contour is indented around .
Frequency response
| ω | |G| | ∠G | Re | Im |
|---|---|---|---|---|
| 0⁺ | ∞ | −90° | −6 | −∞ |
| 0.1 | 19.5 | −107.0° | −5.71 | −18.66 |
| 0.3 | 5.48 | −137.7° | −4.05 | −3.69 |
| 0.5 | 2.53 | −161.6° | −2.40 | −0.80 |
| 0.707 | 1.333 | −180° | −1.333 | 0 |
| 1 | 0.632 | −198.4° | −0.60 | +0.20 |
| ∞ | 0 | −270° | 0 | 0 |
- Low-frequency asymptote: Re → .
- Phase crossover: rad/s.
- Indentation at the origin: maps to an infinite arc clockwise from +90° through 0° to −90°.
- Infinite semicircle: maps to the origin.
.. |
.. |
... |
.. |
... |
... |
.... |
...... |
--------------------------------*****@******------
****** |
**** |
*** |
*** |
** |
*** |
** |
** |
-6 -1.33 0
* w > 0 . w < 0 (mirror) @ point (-1, j0)
crosses at -1.333 (w = 0.707); asymptote Re = -6
Nyquist criterion
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
The plot cuts the negative real axis at −1.333, to the left of −1. Together with its mirror image and the infinite clockwise arc, it encircles twice clockwise: N = 2.
The closed-loop system is unstable, with 2 RHP poles.
The gain must be reduced below 1.5 for stability. Check: gives , so it is unstable. ✓
- 2075 Asoj · 8 marks
Using Nyquist criterion determine the stability of the feedback system whose open loop transfer function is given by G(s)H(s) = (s+5)/[(s−2)(s+2)]. Also find GM.
Answer
Open-loop poles: , so P = 1 (one RHP pole). No poles lie on the -axis.
Frequency response
| ω | Re | Im | |G| | ∠G |
|---|---|---|---|---|
| 0 | −1.25 | 0 | 1.25 | −180° |
| 1 | −1.00 | −0.20 | 1.02 | −168.7° |
| 2 | −0.625 | −0.25 | 0.67 | −158.2° |
| 5 | −0.172 | −0.172 | 0.24 | −135° |
| ∞ | 0 | 0 | 0 | −90° |
- For ω > 0 the plot is in the third quadrant, from −1.25 to the origin (arriving along −90°).
- For ω < 0 it is the mirror image in the second quadrant.
- The infinite semicircle maps to the origin.
|
|
|
|
|
....................... |
.... .....|
... ..
---------*-----@-------------------------*--------
*** **
**** *****|
*********************** |
|
|
|
|
|
-1.25 0
* w > 0 . w < 0 (mirror) @ point (-1, j0)
w = 0 at -1.25; w -> +-inf at origin
Stability
Nyquist criterion: , where = number of open-loop poles in the RHP, = net clockwise encirclements of by the Nyquist plot of , and = number of closed-loop poles in the RHP. The closed loop is stable only if .
As ω goes from −∞ to +∞, the curve runs from the origin through the upper half to −1.25 and back through the lower half. This is a counter-clockwise loop, and it contains −1 because −1.25 < −1. So N = −1.
The closed-loop system is stable. Check: has roots . ✓
Gain margin
Phase crossover is at ω = 0, where .
For this open-loop unstable system, the negative GM means the gain can be reduced by at most a factor of 0.8 (gain is needed) before the system becomes unstable.
Answer: P = 1, N = −1, Z = 0, so the system is stable. GM = 0.8 (−1.94 dB).
- 2074 Asoj · 8 marks
Draw Bode plot for the system with transfer function G(s) = (20s + 200)/[(s² + [?]s + 25)(s² + 40s)]. Determine gain margin, phase margin and comment on stability of the system according to your plot.
Answer
One coefficient in the quadratic is unreadable in the paper ("s² + [?]s + 25"). It is taken here as 4, giving (as in the similar 2072 question). Then rad/s and .
Time-constant form
( dB), type 1.
Corner frequencies and slopes
| Range | Factor added | Slope |
|---|---|---|
| ω < 5 | −20 dB/dec | |
| 5 – 10 | quadratic (ω_n = 5) | −60 dB/dec |
| 10 – 40 | zero at 10 | −40 dB/dec |
| ω > 40 | pole at 40 | −60 dB/dec |
Magnitude asymptotes
| ω | 0.01 | 0.1 | 0.2 | 1 | 5 | 10 | 40 | 100 |
|---|---|---|---|---|---|---|---|---|
| dB | 26.0 | 6.0 | 0 | −14.0 | −28.0 | −46.0 | −70.1 | −94.0 |
The quadratic peak correction at is dB.
Phase
| ω | 0.1 | 0.2 | 1 | 2 | 5 | 5.88 | 10 | 20 | 40 | 100 |
|---|---|---|---|---|---|---|---|---|---|---|
| φ (deg) | −90.5 | −91.0 | −95.2 | −102.4 | −160.6 | −180.0 | −211.0 | −221.1 | −233.2 | −251.6 |
Bode plot
30 |*
| ******
| *******
0 |------------******----------------------------
| ******
| *******
-30 | ****
| ***
| ***
-60 | ****
| ***
| **
-90 | ***
+----------------------------------------------
0.01 0.1 1 10 100
Magnitude asymptotes (dB) vs w (rad/s)
-90 |*************************
| ****
| **
-135 | **
| *
| **
-180 |-------------------------------*--------------
| **
| ****
-225 | *****
| *****
| **
-270 |
+----------------------------------------------
0.01 0.1 1 10 100
Phase (deg); crosses -180 at 5.88 rad/s
Margins
- Gain crossover: the −20 dB/dec line cuts 0 dB at ω = K = 0.2 rad/s (exact 0.200). There φ = −91.0°, so PM = 89.0°.
- Phase crossover: φ = −180° at rad/s, where the exact magnitude is −28.3 dB. So GM = +28.3 dB.
Stability
GM > 0 and PM > 0, and (0.2) < (5.88). The closed-loop system is stable with large margins, though it will be slow because the bandwidth is small.
Answer (with ): GM ≈ 28.3 dB, PM ≈ 89°. The system is stable.
- 2072 Chaitra · 10 marks
Draw Bode plot for the system with transfer function G(s) = (4s + 40)/[(s² + 4s + 25)(s² + 50s)]. Determine gain margin, phase margin and comment on stability of the system according to your plot.
Answer
Time-constant form
- , so dB. Type 1.
- Quadratic: rad/s, . Peak correction dB.
Factors
| Factor | Corner (rad/s) | Slope change | Phase |
|---|---|---|---|
| — | −20 dB/dec | −90° | |
| quadratic, ζ = 0.4 | 5 | −40 dB/dec | 0 to −180° |
| 10 | +20 dB/dec | 0 to +90° | |
| 50 | −20 dB/dec | 0 to −90° |
Magnitude asymptotes
| Range | Slope | Values |
|---|---|---|
| ω < 5 | −20 dB/dec | 30.1 dB at 0.001; 10.1 dB at 0.01; 0 dB at 0.032; −29.9 dB at 1; −43.9 dB at 5 |
| 5 – 10 | −60 dB/dec | −43.9 → −61.9 dB |
| 10 – 50 | −40 dB/dec | −61.9 → −89.9 dB |
| ω > 50 | −60 dB/dec | −108.0 dB at 100 |
Phase
| ω | 0.01 | 0.032 | 0.1 | 1 | 5 | 5.97 | 10 | 50 | 100 |
|---|---|---|---|---|---|---|---|---|---|
| φ (deg) | −90.0 | −90.1 | −90.5 | −94.9 | −159.2 | −180.0 | −208.2 | −231.7 | −246.9 |
Bode plot
45 |
|****
| ********
0 |----------********----------------------------
| ********
| *******
-45 | ******
| ***
| *****
-90 | ***
| **
|
-135 |
+----------------------------------------------
0.001 0.01 0.1 1 10 100
Magnitude asymptotes (dB) vs w (rad/s)
-90 |*****************************
| ****
| **
-135 | **
| *
| **
-180 |----------------------------------*-----------
| **
| *****
-225 | ****
| ***
|
-270 |
+----------------------------------------------
0.001 0.01 0.1 1 10 100
Phase (deg); crosses -180 at 5.97 rad/s
Gain and phase margin
- Gain crossover: on the −20 dB/dec segment, at rad/s. There φ = −90.1°, so
- Phase crossover: φ = −180° at rad/s, where the magnitude is −44.5 dB (asymptote ≈ −48.5 dB, plus the resonance lift). So
Stability
GM ≈ +44.5 dB and PM ≈ +89.9°, both positive, with . The closed-loop system is stable. The very low gain crossover (0.032 rad/s) means the response is very slow; the gain could be raised by about 44 dB (×168) before instability.
Answer: GM ≈ 44.5 dB, PM ≈ 89.9°. The system is stable.
- 2071 Chaitra · 4 marks
State the Nyquist stability criteria for negative feedback control system. Using this concept determine whether the following system represented by figure below is stable. [Figure: open-loop pole-zero plot with poles marked at 3 (drawn on the negative real axis, i.e. s = −3) and at s = +2, and a zero at s = −1. Nyquist diagram: a closed contour crossing the real axis at about −1.25 and 0, extending to about ±1.6 on the imaginary axis, traversed counter-clockwise (arrow at top pointing left), enclosing the −1 point once]
Answer
Nyquist stability criterion
For a negative feedback system with open-loop transfer function :
- = number of open-loop poles in the right half s-plane;
- = net number of clockwise encirclements of the point by the Nyquist plot ( is negative for counter-clockwise encirclements);
- = number of closed-loop poles in the right half-plane.
The closed loop is stable if and only if , i.e. the Nyquist plot must encircle counter-clockwise as many times as there are open-loop RHP poles. If P = 0, it must not encircle −1 at all.
Applying it to the given system
- From the pole-zero plot: open-loop poles at and , and a zero at . So , with P = 1 (the pole at +2).
- From the Nyquist diagram: the plot crosses the real axis at about −1.25 and 0, so the point −1 lies inside the closed curve. The curve is traversed counter-clockwise, so it encircles −1 once anticlockwise: N = −1.
The closed-loop system is stable.
(Consistency check: at ω = 0, gives . Then gives , whose roots are both in the LHP.)
- 2071 Chaitra · 5 marks
Discuss how Bode plot can be used to determine transfer function of the system.
Answer
A Bode plot can be read "backwards" to find the transfer function of a minimum-phase system. The magnitude asymptotes give the gain, type and corner frequencies; the phase plot confirms them.
Procedure
- Draw straight-line asymptotes on the measured magnitude curve, using slopes that are multiples of ±20 dB/decade.
- Initial (low-frequency) slope gives the type:
- 0 dB/dec: type 0 (no pole at the origin);
- −20 dB/dec: one pole at the origin;
- −40 dB/dec: two poles at the origin.
- Find the gain K:
- Type 0: the low-frequency level is .
- Type 1: the −20 dB/dec line (extended if needed) meets 0 dB at ω = K. Equivalently at any point ω on it.
- Type 2: the −40 dB/dec line meets 0 dB at .
- Corner frequencies: at every break in slope:
- −20 dB/dec change: simple pole ;
- +20 dB/dec change: simple zero ;
- −40 dB/dec change: double pole or quadratic , with = corner.
- Damping of a quadratic factor: measure the resonant peak above the asymptote at . Then , or approximately dB at .
- Check with the phase plot: for a minimum-phase system the phase must agree with the factors found. For example, the phase approaches at high frequency. Extra phase lag with no extra magnitude change indicates a transport delay (slope of phase vs ω gives T) or an RHP zero.
- Write the result in time-constant form, then convert to pole-zero form if needed.
Short example
Initial slope −20 dB/dec crossing 0 dB at ω = 10, with a break to −40 dB/dec at ω = 5:
Limitations
The method assumes minimum-phase behaviour, and asymptotes give only approximate corner frequencies. Accurate values come from fitting the exact curve (e.g. −3 dB at a simple-pole corner).
- 2071 Shrawan · 6 marks
Discuss how a Bode plot can be used to determine transfer function of the system. Explain with an example.
Answer
A Bode plot obtained from a frequency-response test can be used to identify the transfer function. The asymptotic magnitude curve gives the gain, type and corner frequencies, and the phase curve confirms them (for a minimum-phase system).
Steps
- Fit asymptotes with slopes of 0, ±20, ±40 … dB/decade to the magnitude curve.
- Low-frequency slope gives the system type: 0, −20 or −40 dB/dec means 0, 1 or 2 integrators.
- Gain K from the low-frequency segment:
- Type 0: .
- Type 1: the extended −20 dB/dec line crosses 0 dB at ω = K.
- Type 2: the −40 dB/dec line crosses 0 dB at .
- Each change of slope is a corner frequency :
- −20 dB/dec change: pole ;
- +20 dB/dec change: zero ;
- −40 dB/dec change: quadratic pole pair. Find ζ from the height of the resonant peak: peak above asymptote ≈ .
- Verify with phase: the phase at very low and very high ω should equal (net poles) at those ends. Unexplained extra lag means a time delay or a non-minimum-phase zero.
Worked example
Suppose the asymptotic magnitude plot is:
- a horizontal line at 20 dB up to ω = 2 rad/s;
- then −20 dB/dec up to ω = 10 rad/s;
- then −40 dB/dec beyond 10 rad/s.
The phase goes from 0° to −180°.
30 |
|******************
| ******
0 |-----------------------****-------------------
| ***
| ****
-30 | ****
| ****
| ****
-60 | ***
| ***
|
-90 |
+----------------------------------------------
0.1 1 10 100 1000
Magnitude asymptotes (dB) vs w (rad/s)
Reading it:
- Initial slope 0 dB/dec, so the system is type 0.
- dB, so K = 10.
- At ω = 2 the slope changes by −20 dB/dec: a pole .
- At ω = 10 the slope changes by a further −20 dB/dec: a pole .
- Phase check: two poles give 0° → −180°, which is consistent.
Check of one point: at ω = 10 the asymptote gives dB. From the TF: dB. ✓ (The true curve is about 3 dB lower at each corner.)
- 2071 Shrawan · 3+3+2 marks
Construct the polar plot of unity feedback system with G(s) = K/[s(s+1)(0.1s+1)]. Then, upgrade the plot to make it Nyquist plot. Hence find range of k for stable operation.
Answer
The polar plot is the locus of in the complex plane as goes from 0 to . The Nyquist plot adds the mirror image for and the map of the small indentation around the pole at the origin, so that the whole Nyquist contour is mapped.
Polar plot
| Magnitude | Phase | |
|---|---|---|
| 0 |
- Low-frequency asymptote: as , . The plot starts at infinity parallel to the negative imaginary axis, along the line .
- Negative real axis crossing: set phase : rad/s.
So the plot crosses the negative real axis at and ends at the origin, tangent to the positive imaginary axis ().
Im
|
-K/11 |
----o-------+--------> Re
/ \_____/|
| w=3.16 |
| |
| w ->0+ (to -inf j,
| asymptote Re=-1.1K)
Nyquist plot
- Draw the polar plot for (third quadrant, crosses at , ends at origin).
- Draw its mirror image about the real axis for .
- The infinite semicircle of the Nyquist contour (, ) maps to the origin.
- The small semicircle around the pole at (, ) maps to , i.e. an infinite-radius semicircle traversed clockwise from to through the positive real axis.
The resulting closed curve is the Nyquist plot. It cuts the negative real axis only at .
Range of K for stability
Nyquist criterion: , where = open-loop RHP poles, = clockwise encirclements of .
- (poles at ; the origin pole is excluded by the indentation).
- For stability, , so : the point must not be enclosed, i.e. it must lie to the left of the crossing point.
If , the curve encircles twice clockwise (, ): unstable. At the system oscillates at rad/s.
Check by Routh: gives .
Answer: The closed-loop system is stable for .
- 2070 Chaitra (old course) · 8 marks
Find the Gain Margin and Phase Margin using Bode plots for the following transfer function: G(s) = 1/[s(0.1s+1)(0.2s+1)].
Answer
Type-1 system, , corner frequencies rad/s and rad/s.
Magnitude plot (asymptotic)
| Range of | Slope |
|---|---|
| dB/dec (pole at origin) | |
| dB/dec | |
| dB/dec |
- At : dB; at : 0 dB.
- At : dB.
- At : dB.
- At : dB.
Phase plot
| (rad/s) | 0.1 | 1 | 2 | 5 | 7.07 | 10 | 20 | 100 |
|---|---|---|---|---|---|---|---|---|
dB
20 |\ -20dB/dec
0 |-\---------------------- w
| \ wgc~1
-14 | \___ w=5 -40
-26 | \__ w=10
| \ -60
deg
-90 |--__
-180 |-------x---------- wpc=7.07
-270 | ----___
Phase crossover frequency and gain margin
At , : .
Gain crossover frequency and phase margin
From the asymptotic plot, the magnitude is 0 dB at rad/s. Solving exactly gives rad/s.
(Using the asymptotic value : .)
Answer: GM = 23.5 dB at rad/s; PM ≈ 73.4° at rad/s. Both margins are positive, so the closed-loop system is stable.
- 2070 Chaitra (old course) · 8 marks
An engineer is called in to consult on a control system in a piece of equipment in the field. No one can find the design report or test results from the original design of control system. The engineer therefore decided to take a frequency response of the system. The resulting asymptotic frequency response is obtained as below. Determine the transfer function. [Figure: asymptotic magnitude plot; 40 dB at ω = 0.1 with slope −20 dB/dec; at ω = √2 there is a resonant peak 4 dB above the asymptote, after which the slope is −60 dB/dec; the curve crosses 0 dB at ω = 2 where the slope changes to −40 dB/dec; at ω = 3 the slope changes to −60 dB/dec]
Answer
We read the asymptotic plot from left to right: each change of slope is a corner frequency, and the low-frequency line fixes the gain.
Step 1: Initial slope and gain
The initial slope is dB/dec, so there is one pole at the origin (type-1). Its line is :
Step 2: Corner at (complex poles)
The slope changes from to dB/dec, a change of dB/dec, and the curve shows a resonant peak. So there is a pair of complex poles with rad/s.
The exact curve at the corner lies above the asymptote, so
Quadratic factor:
Step 3: Corner at (zero)
Slope changes from to dB/dec (+20 dB/dec), so there is a simple zero at : factor .
Step 4: Corner at (pole)
Slope changes from to dB/dec (−20 dB/dec), so there is a simple pole at : factor .
Transfer function
Check: as , , which gives 40 dB at as required.
| Corner | Factor | Slope after |
|---|---|---|
| — | dB/dec | |
| complex poles, | dB/dec | |
| 2 | zero | dB/dec |
| 3 | pole | dB/dec |
Note: with the straight-line asymptote is about 8 dB at , not exactly 0 dB as labelled in the sketch; the gain is taken from the clearly marked low-frequency point (40 dB at ), which is the usual method.
Answer: , with and rad/s for the complex poles.
- 2070 Chaitra · 4 marks
Discuss how Bode plot is used for determining relative stability.
Answer
Relative stability tells how far a stable system is from becoming unstable. On a Bode plot it is measured by the gain margin (GM) and phase margin (PM), read directly from the magnitude and phase curves of the open-loop transfer function .
Procedure
- Draw the magnitude plot (dB) and phase plot of on the same frequency axis.
- Gain crossover frequency : where the magnitude curve crosses 0 dB.
- Phase crossover frequency : where the phase curve crosses .
- Gain margin:
i.e. the distance of the magnitude curve below 0 dB at . 5. Phase margin:
i.e. the distance of the phase curve above at .
dB |\
0 |-\----------+-------- w
| \ wgc | ^ GM
| \ | v
deg | |
-180 |----+-------x-------- w
| ^ PM wpc
Interpretation (minimum-phase systems)
| Condition | Closed-loop system |
|---|---|
| GM > 0 dB and PM > 0°, i.e. | Stable |
| GM = 0 dB, PM = 0°, | Marginally stable (sustained oscillation) |
| GM < 0 dB or PM < 0°, i.e. | Unstable |
- Larger margins mean more relative stability. GM tells by how much the gain can be increased before instability; PM tells how much extra phase lag (e.g. a time delay) can be added.
- Good design values: GM ≥ 6 dB and PM of about 30°–60°.
- PM is linked to damping: approximately for PM below about 70°. Small PM means a large overshoot.
Example: for a system with rad/s, phase there, and magnitude dB at : PM = 30°, GM = 10 dB, so the system is stable with reasonable margin.
- 2069 Chaitra · 10 marks
Draw the bode plot for transfer function G(s) = 48(1+s)/[s²(1+3s)(1+0.5s)(2+0.2s)]; from the graph determine (i) Phase crossover frequency (ii) Gain crossover frequency (iii) P.M (iv) G.M (v) Stability of the system.
Answer
Step 1: Time-constant form
- , type-2 (double pole at origin): initial slope dB/dec.
- Corner frequencies: pole , zero , pole , pole rad/s.
Step 2: Asymptotic magnitude plot
| Range | Factor added | Net slope |
|---|---|---|
| dB/dec | ||
| – | pole | dB/dec |
| – | zero | dB/dec |
| – | pole | dB/dec |
| pole | dB/dec |
Step 3: Phase plot
| 0.1 | 0.2 | 0.5 | 1 | 2 | 4 | 10 | |
|---|---|---|---|---|---|---|---|
dB 67 |\ -40
46 | \__ -60
18 | \__ -40
6 | \__ -60
0 |-----------x-------- w
wgc~2.5
deg -180|------------------- w
|\___
| \____ (always
| \__ below -180)
(i) Phase crossover frequency
for every , so the phase is always below ; it starts at only as . The phase curve never crosses at a finite non-zero frequency, so does not exist (it is at ).
(ii) Gain crossover frequency
From the asymptotic plot, slope after (6 dB): rad/s. The exact value from is rad/s.
(iii) Phase margin
(iv) Gain margin
Since the phase never reaches from above and the magnitude is very large at low frequency, GM is negative (−∞ dB): reducing the gain cannot bring the phase above .
(v) Stability
PM is negative and GM is negative, so the closed-loop system is unstable. Check: the characteristic equation has roots in the right half plane.
Answer: – none (phase always below −180°); rad/s (2.5 rad/s asymptotic); PM ≈ −77.6°; GM negative; closed loop unstable.
- 2068 Chaitra · 4 marks
Write a short note on gain margin and phase margin.
Answer
Gain margin and phase margin are measures of relative stability: they show how close the closed-loop system is to instability, using the open-loop frequency response .
Gain margin (GM)
The factor by which the open-loop gain can be increased before the closed-loop system becomes marginally stable.
- = phase crossover frequency, where .
- On the polar plot: if the curve cuts the negative real axis at , then .
Phase margin (PM)
The additional phase lag that can be added at the gain crossover frequency before the system becomes marginally stable.
- = gain crossover frequency, where (0 dB).
Im
| unit circle
----+----
/ | \
-1 o----+------+--- Re
\ PM /|
\_/ | GM = 1/a
Stability from margins
| GM, PM | System |
|---|---|
| both positive | stable |
| both zero | marginally stable |
| negative | unstable |
- Typical good values: GM ≥ 6 dB, PM 30°–60°.
- Larger PM means less overshoot (PM ≈ 100ζ approx).
Example: if at then GM dB; if at then PM .
- 2068 Baisakh (old course) · 8 marks
Draw bode plot of a system having open loop transfer function G(s) = 4(s+4)/[(s+2)(s²+2s+4)]. Also analyze the stability.
Answer
Step 1: Time-constant (Bode) form
- : dB, type-0 (initial slope 0 dB/dec).
- Simple pole: corner rad/s.
- Quadratic poles: rad/s, (corner 2 rad/s).
- Simple zero: corner rad/s.
Step 2: Asymptotic magnitude plot
| Range | Slope | Value at end |
|---|---|---|
| 0 dB/dec | 6.02 dB | |
| dB/dec | dB | |
| dB/dec | at : dB |
Corrections at : quadratic with gives 0 dB, the simple pole dB, the zero dB, so the actual value there is dB.
Step 3: Phase plot
| (rad/s) | 0.1 | 0.5 | 1 | 2 | 2.59 | 4 | 10 |
|---|---|---|---|---|---|---|---|
| $ | G | $ (dB, exact) | 6.02 | 6.09 | 6.22 | 3.98 | 0 |
dB 6 |------\ 0 dB/dec
0 |-------\-------------- w
| 2 \ -60
-12 | \__ 4
| \__ -40
deg 0|--__
-90 | \__
-180 |- - - - -\____________ (approaches -180)
Step 4: Margins
- Gain crossover: the asymptote gives rad/s; the exact value is rad/s.
- Phase crossover: the net phase goes from toward (three poles , one zero ) and reaches only at . So and
Stability
All open-loop poles and zeros are in the left half plane (minimum phase), GM and PM , so the closed-loop system is stable, with a reasonable phase margin (moderate overshoot, ).
Answer: rad/s, PM ≈ 43°, GM = ∞; the closed-loop system is stable.
- 2066 Bhadra (old course) · 8 marks
Use Nyquist stability criteria to evaluate the stability of the system with open loop transfer function G(s) = 10/[s(s²+2s+4)]. Identify phase cross-over frequency and gain margin from the Nyquist plot.
Answer
Frequency response
| 0+ | 0.5 | 1 | 1.5 | 2 | 3 | 5 | ||
|---|---|---|---|---|---|---|---|---|
| $ | G | $ | 5.15 | 2.77 | 1.92 | 1.25 | 0.43 | |
- Low-frequency asymptote: as .
Phase crossover frequency
The imaginary part of the denominator is zero when :
So the plot cuts the negative real axis at .
Nyquist plot
Im
w<0 mirror |
____ |
/ \ |
----o--x---+----+----- Re
-1.25 -1 \__/ |
w=2 |
w->0+ : to -inf j
(asymptote Re=-1.25)
small semicircle at s=0 maps
to infinite arc, clockwise
- : starts at , passes through at , ends at the origin at .
- : mirror image.
- Indentation around the pole at maps to an infinite semicircle clockwise (through the positive real axis).
- Infinite semicircle of the -plane maps to the origin.
Nyquist criterion
- (open-loop poles: , ; none in the RHP).
- The crossing at lies to the left of , so the point is encircled twice clockwise: .
- closed-loop poles in the RHP.
The closed-loop system is unstable. (Check by Routh: : , two sign changes.)
Gain margin
The negative GM confirms instability; the gain must be reduced below for stability.
Answer: rad/s, GM = 0.8 (−1.94 dB); N = 2, Z = 2, so the closed-loop system is unstable.
- 2066 Jestha (old course) · 6 marks
Draw the asymptotic Bode magnitude plot of the unity feedback system whose open loop transfer function is given by G(s) = 125/[s(s²+10s+25)].
Answer
Time-constant form
- , type-1: initial slope dB/dec.
- : rad/s, (critically damped, i.e. two equal real poles at ).
- Corner frequency rad/s; after it the slope falls by 40 dB/dec.
Asymptotic magnitude
| Factor | Corner | Slope contributed |
|---|---|---|
| — | dB constant | |
| — | dB/dec (passes 0 dB at ) | |
| 5 rad/s | dB/dec after 5 |
| Range | Net slope |
|---|---|
| dB/dec | |
| dB/dec |
Points on the asymptotic plot:
dB
34 |\
| \ -20 dB/dec
14 | \ (w=1)
0 |------\-------------- w (log)
| 5 \
-18 | \ (w=10)
| \ -60 dB/dec
-60 | \ (w=50)
0.1 1 5 10 50
Correction (optional)
For the exact curve at the corner is dB below the asymptote, so the actual magnitude at is dB (exact values: 13.64 dB at , dB at ).
The asymptotic gain crossover frequency is rad/s.
Answer: straight line of −20 dB/dec through 13.98 dB at ω = 1, meeting 0 dB at the corner ω = 5 rad/s, then −60 dB/dec.
- 2066 Jestha (old course) · 10 marks
Use Nyquist stability criterion to find the range of K for which the unity feedback system represented by open loop transfer function G(s) = K/[s(s+1)(s+2)] is stable.
Answer
Frequency response
| 0.5 | 1 | 2 | ||||
|---|---|---|---|---|---|---|
| $ | G | /K$ | 0.868 | 0.316 | 0.167 | |
Key points of the plot
- Low-frequency asymptote: as .
- Negative real-axis crossing: imaginary part of denominator zero: rad/s.
- As , at .
Nyquist plot
Im
w<0 mirror|
___ |
/ \ |
--o-----+---+------- Re
-K/6 \_/ |
w=1.414 |
w->0+: to -inf j along Re=-0.75K
pole at s=0 -> infinite arc,
clockwise from w=0- to w=0+
- : polar plot above.
- : mirror image about the real axis.
- Small indentation at maps to an infinite clockwise semicircle.
- Infinite -semicircle maps to the origin.
Applying the criterion
with (poles at ).
- If : lies outside the plot, , : stable.
- If : is encircled twice clockwise, , : unstable.
- If : the plot passes through : marginally stable, oscillation at rad/s.
Check by Routh: requires , i.e. .
Answer: the closed-loop system is stable for ; at it oscillates at 1.414 rad/s.
- 2081 Bhadra · 7+1 marks
Draw the Bode plot of the unity feedback system with an open loop transfer function G(s) = 1000/[s(1+0.1s)(1+0.001s)]. Also comment on stability.
Answer
Factors and corner frequencies
- (60 dB), one pole at origin: initial slope dB/dec.
- Corner frequencies: rad/s, rad/s.
Asymptotic magnitude plot
| Range | Slope |
|---|---|
| dB/dec | |
| dB/dec | |
| dB/dec |
Phase plot
| 1 | 10 | 50 | 100 | 1000 | ||
|---|---|---|---|---|---|---|
dB 60 |\ -20
40 | \___ w=10
0 |-------\---------------- w
| w=100\ -40
-40 | \__ w=1000
| \ -60
deg |
-90 |--__
-180 |-------x----------------
| 100 \___
-270 | ----
1 10 100 1000 1e4
Crossover frequencies and margins
- Phase crossover: rad/s.
- Gain crossover: the asymptote gives 0 dB at rad/s; exactly rad/s, where .
Comment on stability (1 mark)
and almost coincide, and GM ≈ 0 dB, PM ≈ 0°. The closed-loop system is just stable (on the verge of instability, practically marginally stable): its dominant poles are at , giving a very lightly damped oscillation at about 100 rad/s. Any small increase in gain makes it unstable. Routh check: : , so stable by a very small margin. A compensator (e.g. lead) is needed for acceptable relative stability.
Answer: rad/s, GM ≈ 0.09 dB, PM ≈ 0.06°: the system is barely (marginally) stable.
- 2081 Baisakh · 8 marks
Using Nyquist criterion determine the stability of the feedback system whose open loop transfer function is given by G(s)H(s) = 60/[(s+1)(s+2)(s+5)].
Answer
Open-loop poles
has poles at : none in the right half plane, so . There is no pole on the axis, so no indentation is needed.
Frequency response
Denominator: . With :
| 0 | 0.5 | 1.118 | 2 | 2.84 | 4.123 | 10 | ||
|---|---|---|---|---|---|---|---|---|
| $ | GH | $ | 6 | 5.18 | 3.41 | 1.76 | 1.0 | 0.476 |
Axis crossings
- Imaginary axis (real part of denominator zero): rad/s, .
- Negative real axis (imaginary part zero): rad/s.
Nyquist plot
Im
w<0 | ___
___|_/ \
----o--x--+---+------o--- Re
-1 -0.476 | 6 (w=0)
\___|_ /
| \__/ w>0
| -j3.41
- : starts at , goes through , cuts the negative real axis at , reaches the origin at .
- : mirror image.
- Infinite semicircle of the -plane maps to the origin.
Nyquist criterion
. The plot cuts the real axis at , to the right of , so the point is not encircled: .
No closed-loop poles in the RHP, so the closed-loop system is stable.
Relative stability: (6.44 dB), PM ≈ 25° at rad/s. The system becomes unstable if the gain 60 is raised above (Routh: ).
Answer: N = 0, P = 0, Z = 0 – the closed-loop system is stable (GM ≈ 6.4 dB).
- 2080 Baisakh · 8 marks
What is Nyquist Contour? Map the Nyquist contour of open loop transfer function G(s) = 300/[(s+3)(s+1)(s+2)] into G(s) plane and apply Nyquist criterion to check the stability of closed loop system.
Answer
Nyquist contour
The Nyquist contour is a closed path in the -plane that encloses the entire right half plane. It runs up the whole axis from to and returns along a semicircle of infinite radius, traversed clockwise. If has poles on the axis, the contour goes around them by small semicircles of radius so they are not on the path.
jw
|\ +j inf
| \
| \ R -> inf
-----+---)----- sigma
| / (clockwise)
| /
|/ -j inf
Mapping this contour through gives the Nyquist plot; by the principle of the argument, (clockwise encirclements of ), so .
Mapping
Poles at : , none on the axis.
Section I ():
| 0 | 0.5 | 1 | 2 | 3.317 | 5 | ||
|---|---|---|---|---|---|---|---|
| $ | G | $ | 50 | 42.8 | 30 | 13.2 | 5.0 |
- Imaginary-axis crossing: , .
- Real-axis crossing: , .
Section II (infinite semicircle, ): ; maps to the origin.
Section III (): mirror image of section I about the real axis.
Im
| ___ w<0
_____|__/ \
--o--o--+----+-------o--- Re
-5 -1 \____|__ / 50
w=3.317 | \__/ w>0
| -j30 (w=1)
Nyquist criterion
The plot crosses the negative real axis at , to the left of . Following the curve, the point is encircled twice in the clockwise direction: .
Two closed-loop poles lie in the right half plane, so the closed-loop system is unstable. (Check: has roots and .) GM ( dB); the gain must be below for stability.
Answer: N = 2, P = 0, Z = 2 – the closed-loop system is unstable.
- 2078 Bhadra · 8 marks
Using Nyquist criteria, determine the stability of the feedback system whose OLTF is given by G(s)H(s) = 1/[s²(1+2s)(1+s)].
Answer
Open-loop data
Poles: double pole at (type-2), and , . No poles in the RHP: . The double pole at the origin is bypassed by a small semicircle in the Nyquist contour.
Section I:
| 0.2 | 0.4 | 0.707 | 1 | 2 | |||
|---|---|---|---|---|---|---|---|
| $ | GH | $ | 22.8 | 4.53 | 0.943 | 0.316 | |
- The phase is always below , so the plot lies in the second quadrant at low frequency. For small : (real part , imaginary part ).
- It cuts the positive imaginary axis where , at .
- It then enters the first quadrant and reaches the origin at .
- It never cuts the negative real axis for finite .
Section II: infinite semicircle
, : , maps to the origin.
Section III:
Mirror image of section I (third and fourth quadrants).
Section IV: indentation at the origin
, :
Angle goes from to : a circle of infinite radius, 360° clockwise (two half circles), through the positive real axis.
Im
w>0 | j0.943
(from -inf|+j inf)
\_______|__
| \_ to origin
----x------+------ Re
-1 | _/
_______|_/
/ w<0 |
plus a full infinite
clockwise circle at w=0
Nyquist criterion
The point lies between the branch (above it) and the branch (below it), and the 360° infinite clockwise arc closes the curve around it. So is encircled twice clockwise: .
The closed-loop system has two poles in the RHP and is unstable.
Check by Routh: . The term is missing, so the system cannot be stable; the roots are and (two in the RHP). A type-2 system with only extra lags needs a zero (lead action) to be stabilised.
Answer: P = 0, N = 2, Z = 2 – the closed-loop system is unstable for any positive gain.
- 2076 Chaitra · 3 marks
Write a short note on Nyquist stability criterion.
Answer
The Nyquist stability criterion is a graphical frequency-domain method that finds the number of closed-loop poles in the right half -plane from the plot of the open-loop transfer function . It is based on Cauchy's principle of the argument.
Statement
If the Nyquist contour (the whole axis plus an infinite semicircle enclosing the RHP, traversed clockwise) is mapped through , then
- = number of open-loop poles in the RHP
- = number of closed-loop poles (zeros of ) in the RHP
- = number of clockwise encirclements of the critical point
The closed-loop system is stable only if , i.e. (the plot encircles anticlockwise times). For an open-loop stable system (): stable if the Nyquist plot does not encircle .
Steps
- Find from the open-loop poles.
- Plot for , add its mirror image, and close it (poles at origin give infinite clockwise arcs).
- Count around , compute .
Merits
- Works with experimental frequency-response data.
- Handles time delay and open-loop unstable systems.
- Gives relative stability (gain and phase margins) as well.
Example: cuts the real axis at ; , , so : stable.
- 2076 Chaitra · 8 marks
Sketch the polar plot of the system whose open loop transfer function is given by G(s)H(s) = 1/[s(1+s)(1+2s)]. Also comment on stability.
Answer
Frequency response
Rationalised form:
| (rad/s) | 0.2 | 0.4 | 0.5 | 0.707 | 1 | 2 | ||
|---|---|---|---|---|---|---|---|---|
| $ | GH | $ | 4.55 | 1.81 | 1.26 | 0.667 | 0.316 | |
Key points
- Start (): magnitude at . The real part tends to , so the plot comes from along the asymptote .
- Negative real-axis crossing: imaginary part zero when rad/s.
- End (): magnitude 0 at ; the plot reaches the origin tangent to the positive imaginary axis.
Im
|
-0.667 |
----x--o-----+--------- Re
-1 |\_/ | (ends at origin
| w=0.707 from 2nd quad.)
___| |
/ | |
| Re=-3 asymptote
| w -> 0+
v -j inf
Comment on stability
- Open-loop poles: , so .
- The polar plot cuts the negative real axis at , which is to the right of ; with its mirror image and the infinite clockwise arc for the pole at the origin, the point is not encircled: , .
The closed-loop system is stable.
Relative stability:
The margins are small, so the response will be quite oscillatory; the gain can be raised by a factor of 1.5 before instability (Routh: needs ).
Answer: the plot crosses the negative real axis at −0.667 (ω = 0.707 rad/s); the closed-loop system is stable with GM = 1.5 (3.5 dB) and PM ≈ 11°.
Questions from Old Question Collection (EE 602) (IOE Control System exam papers (EE 602 and older course), 2065 to 2082) and Old Question Collection (BEI, EE 504) (IOE BEI Control System (EE 504) exam papers, 2076 to 2081). Answers are written for this site; check them against your class notes.
Chapter titles and hours from the IOE syllabus ↗