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Chapter 4 · 4 hours

Stability

IOE past exam questions

Past questions and answers

29 questions set from this chapter, 3 of them more than once. Most asked first.

  • Asked 5 times
  • 2079 Bhadra · 8 marks
  • 2074 Asoj · 8 marks
  • 2071 Chaitra · 4 marks
  • 2069 Chaitra · 6 marks
  • 2081 Baisakh · 6 marks

Construct Routh array and determine the stability of the system whose characteristic equation is s⁶ + 3s⁵ + 4s⁴ + 6s³ + 5s² + 3s + 2. Comment on the location of the roots of characteristic equation.

Answer

Result: the system is unstable. It has 2 roots in the LHP, a repeated pair on the jωj\omega axis at ±j1\pm j1, and no roots in the RHP.

The Routh–Hurwitz criterion states that the number of roots in the right half of the s-plane equals the number of sign changes in the first column of the Routh array. A row of all zeros means there are roots placed symmetrically about the origin; these are found from the auxiliary equation.

q(s)=s6+3s5+4s4+6s3+5s2+3s+2=0q(s) = s^6+3s^5+4s^4+6s^3+5s^2+3s+2 = 0

All coefficients are present and positive, so the necessary condition is satisfied.

Routh array

RowCol 1Col 2Col 3Col 4
s6s^61452
s5s^53630
s4s^43(4)−1(6)3=2\frac{3(4)-1(6)}{3}=23(5)−1(3)3=4\frac{3(5)-1(3)}{3}=42
s3s^300

The s3s^3 row is all zeros. Auxiliary equation from the s4s^4 row:

A(s)=2s4+4s2+2,dAds=8s3+8sA(s) = 2s^4+4s^2+2, \qquad \frac{dA}{ds} = 8s^3 + 8s

Replace the s3s^3 row by 8, 88,\ 8 and continue:

RowCol 1Col 2Col 3
s3s^388
s2s^28(4)−2(8)8=2\frac{8(4)-2(8)}{8}=28(2)−2(0)8=2\frac{8(2)-2(0)}{8}=2
s1s^10

The s1s^1 row is zero again. New auxiliary equation A1(s)=2s2+2A_1(s) = 2s^2+2, dA1ds=4s\frac{dA_1}{ds} = 4s:

RowCol 1
s1s^14
s0s^02

First column: 1, 3, 2, 8, 2, 4, 21,\ 3,\ 2,\ 8,\ 2,\ 4,\ 2. No sign change, so no root is in the right half plane.

Roots of the auxiliary equation

2s4+4s2+2=2(s2+1)2=0  ⇒  s=±j1, ±j12s^4+4s^2+2 = 2(s^2+1)^2 = 0 \;\Rightarrow\; s = \pm j1,\ \pm j1

So ±j1\pm j1 is a repeated pair on the imaginary axis. Dividing q(s)q(s) by (s2+1)2(s^2+1)^2 leaves s2+3s+2=(s+1)(s+2)s^2+3s+2 = (s+1)(s+2).

Location of roots

RegionNumberRoots
Right half plane0none
On jωj\omega axis4±j1\pm j1 (each twice)
Left half plane2−1, −2-1,\ -2

Comment on stability

There is no RHP root, but the imaginary-axis roots are repeated. Repeated poles on the jωj\omega axis give terms like tsin⁡tt\sin t in the response, which grow without limit. Therefore the system is unstable. If the jωj\omega roots were non-repeated, it would only be marginally stable.

  • Asked 2 times
  • 2075 Asoj · 4 marks
  • 2079 Bhadra · 8 marks

Using R-H criteria, tell how many roots of polynomial are in right half s-plane, in left half s-plane and on jω axis. Comment on stability. s⁵ + 4s⁴ + 2s³ + 8s² + s + 4 = 0

Answer

Result: RHP = 0, LHP = 1 (at s=−4s=-4), jωj\omega axis = 4 (±j1\pm j1, each twice). The system is unstable.

The number of sign changes in the first column gives the RHP roots. A zero row gives the roots that are symmetric about the origin; these are found from the auxiliary polynomial.

s5+4s4+2s3+8s2+s+4=0s^5+4s^4+2s^3+8s^2+s+4=0

Routh array

RowCol 1Col 2Col 3
s5s^5121
s4s^4484
s3s^34(2)−1(8)4=0\frac{4(2)-1(8)}{4}=04(1)−1(4)4=0\frac{4(1)-1(4)}{4}=0

The s3s^3 row is all zeros. Auxiliary polynomial from the s4s^4 row:

A(s)=4s4+8s2+4,dAds=16s3+16sA(s) = 4s^4+8s^2+4, \qquad \frac{dA}{ds} = 16s^3+16s
RowCol 1Col 2
s3s^31616
s2s^216(8)−4(16)16=4\frac{16(8)-4(16)}{16}=416(4)−016=4\frac{16(4)-0}{16}=4
s1s^10 (zero row again)

New auxiliary polynomial A1(s)=4s2+4A_1(s)=4s^2+4, dA1ds=8s\frac{dA_1}{ds}=8s:

RowCol 1
s1s^18
s0s^04

First column: 1, 4, 16, 4, 8, 41,\ 4,\ 16,\ 4,\ 8,\ 4. No sign change, so there is no root in the RHP.

Roots from the auxiliary polynomial

4s4+8s2+4=4(s2+1)2=0⇒s=±j1, ±j14s^4+8s^2+4 = 4(s^2+1)^2 = 0 \Rightarrow s=\pm j1,\ \pm j1

These 4 roots lie on the jωj\omega axis (repeated pair). The remaining root: s5+4s4+2s3+8s2+s+4(s2+1)2=s+4\frac{s^5+4s^4+2s^3+8s^2+s+4}{(s^2+1)^2} = s+4, so s=−4s=-4.

RegionNumber of roots
Right half s-plane0
Left half s-plane1 (s=−4s=-4)
On jωj\omega axis4 (±j1\pm j1 repeated)

Stability

No root is in the RHP, but the roots on the jωj\omega axis are repeated. They produce a response term like tsin⁡tt\sin t, which grows with time. So the system is unstable.

  • Asked 2 times
  • 2074 Chaitra · 3 marks
  • 2072 Chaitra · 4 marks

Explain how RH (Routh Hurwitz) method is used for determining relative stability.

Answer

Relative stability tells how far the closed-loop poles lie to the left of the imaginary axis, i.e. how stable a stable system is. The basic Routh–Hurwitz test only checks for poles on or right of the jωj\omega axis. To find out whether all roots lie to the left of a line s=−σs=-\sigma, the axis is shifted.

Method (axis shifting)

  1. Take the characteristic equation q(s)=0q(s)=0.
  2. Substitute s=z−σs = z - \sigma, where σ>0\sigma>0 is the required margin. This moves the vertical line s=−σs=-\sigma to the new imaginary axis (z=0z=0).
  3. Expand to get a polynomial q(z)q(z).
  4. Form the Routh array of q(z)q(z).
    • Number of sign changes = number of roots to the right of s=−σs=-\sigma.
    • No sign change: all roots lie to the left of s=−σs=-\sigma, so every root has real part more negative than −σ-\sigma. Each mode then decays at least as fast as e−σte^{-\sigma t}.
    • A zero row: roots lie exactly on the line s=−σs=-\sigma.
  5. Repeat for other σ\sigma values, or keep σ\sigma (or a gain KK) as a variable to find the limit.
          jw   |  jw' (new axis)
               |   |
     x         |   |
        x      |   |        Shift: s = z - sigma
   ------------+---+-------- sigma
     x       -sigma 0
               |   |

Example

q(s)=s3+6s2+11s+6q(s)=s^3+6s^2+11s+6 (roots −1,−2,−3-1, -2, -3). Check whether all roots lie left of s=−0.5s=-0.5. Put s=z−0.5s=z-0.5:

q(z)=z3+4.5z2+5.75z+1.875q(z) = z^3 + 4.5z^2 + 5.75z + 1.875
RowCol 1Col 2
z3z^315.75
z2z^24.51.875
z1z^15.333
z0z^01.875

No sign change, so all roots lie to the left of s=−0.5s=-0.5. With s=z−1s=z-1, q(z)=z3+3z2+2zq(z) = z^3+3z^2+2z; the constant term becomes zero, showing a root exactly at s=−1s=-1.

Uses

  • Ensures a minimum decay rate, i.e. settling time ts≈4/σt_s \approx 4/\sigma.
  • Lets the designer find the range of gain KK that keeps all poles left of a chosen line.
  • 2078 Kartik · 4 marks
  • 2078 Kartik · 8 marks

The characteristic equation of a feedback control system is s⁴ + 20s³ + 15s² + 2s + K = 0. (i) Determine the range of K for the system to be stable. (ii) Can the system be marginally stable? If so, find the required value of K and the frequency of sustained oscillation.

Answer

Apply the Routh array with KK in it. For stability, every element of the first column must be positive. Marginal stability occurs when the s1s^1 row becomes zero.

s4+20s3+15s2+2s+K=0s^4+20s^3+15s^2+2s+K = 0

Routh array

RowCol 1Col 2Col 3
s4s^4115KK
s3s^32020
s2s^220(15)−1(2)20=14.9\frac{20(15)-1(2)}{20}=14.9KK
s1s^114.9(2)−20K14.9=29.8−20K14.9\frac{14.9(2)-20K}{14.9}=\frac{29.8-20K}{14.9}0
s0s^0KK

(i) Range of K for stability

  • From s1s^1 row: 29.8−20K>0⇒K<1.4929.8 - 20K > 0 \Rightarrow K < 1.49
  • From s0s^0 row: K>0K > 0
0<K<1.490 < K < 1.49

(ii) Marginal stability

Yes. At K=1.49K = 1.49 the s1s^1 row becomes all zero, and the system has a pair of roots on the jωj\omega axis (marginally stable, sustained oscillation).

Auxiliary equation from the s2s^2 row:

14.9s2+K=014.9s2+1.49=0s2=−0.1⇒s=±j0.316\begin{aligned} 14.9s^2 + K &= 0 \\ 14.9s^2 + 1.49 &= 0 \\ s^2 &= -0.1 \Rightarrow s = \pm j0.316 \end{aligned}

So the frequency of sustained oscillation is ω=0.1=0.316\omega = \sqrt{0.1} = 0.316 rad/s.

Answer: stable for 0<K<1.490 < K < 1.49; marginally stable at Kmar=1.49K_{mar} = 1.49, oscillating at ω=0.316\omega = 0.316 rad/s.

  • 2082 Baisakh · 6 marks

A unity feedback system has the feedforward transfer function G(s) = K(s+1)/(s³+bs²+3s+1). Using R-H Criterion, find the range of K for the system to be stable. When does the system just oscillate and what would be that frequency during sustained oscillation?

Answer

Result: stable for K>−1K>-1 and b(3+K)>1+Kb(3+K)>1+K. For K>0K>0 this means any KK when b≥1b\ge1, and 0<K<3b−11−b0<K<\frac{3b-1}{1-b} when 13<b<1\frac13<b<1. It just oscillates at K=3b−11−bK=\frac{3b-1}{1-b}, with ω=3+K=21−b\omega=\sqrt{3+K}=\sqrt{\frac{2}{1-b}} rad/s.

The characteristic equation is 1+G(s)=01+G(s)=0. The Routh array gives the stability conditions in terms of KK and bb. Sustained oscillation occurs when the s1s^1 row becomes zero.

Characteristic equation

s3+bs2+3s+1+K(s+1)=0s3+bs2+(3+K)s+(1+K)=0\begin{aligned} s^3+bs^2+3s+1 + K(s+1) &= 0 \\ s^3 + bs^2 + (3+K)s + (1+K) &= 0 \end{aligned}

Routh array

RowCol 1Col 2
s3s^313+K3+K
s2s^2bb1+K1+K
s1s^1b(3+K)−(1+K)b\frac{b(3+K)-(1+K)}{b}0
s0s^01+K1+K

Conditions for stability

  1. b>0b > 0
  2. 1+K>0⇒K>−11+K>0 \Rightarrow K>-1
  3. b(3+K)−(1+K)>0⇒K(b−1)>1−3bb(3+K) - (1+K) > 0 \Rightarrow K(b-1) > 1-3b

Interpreting condition 3 (for K>0K>0, b>0b>0):

  • If b≥1b \ge 1: condition 3 holds for every K>0K>0, so the system is stable for all K>0K>0.
  • If b<1b < 1: K<3b−11−bK < \dfrac{3b-1}{1-b}. A positive range exists only if b>13b > \frac{1}{3}.
Range: 0<K<3b−11−b(13<b<1)\text{Range: } 0 < K < \frac{3b-1}{1-b}\quad\left(\tfrac13<b<1\right)

Sustained oscillation

The system just oscillates when the s1s^1 row is zero:

b(3+K)=1+K⇒Kmar=3b−11−bb(3+K) = 1+K \quad\Rightarrow\quad K_{mar} = \frac{3b-1}{1-b}

Auxiliary equation from the s2s^2 row:

bs2+(1+K)=0ω2=1+Kb=3+K=21−bω=21−b rad/s\begin{aligned} bs^2 + (1+K) &= 0 \\ \omega^2 &= \frac{1+K}{b} = 3+K = \frac{2}{1-b} \\ \omega &= \sqrt{\frac{2}{1-b}}\ \text{rad/s} \end{aligned}

Example: for b=0.5b = 0.5: Kmar=0.50.5=1K_{mar} = \frac{0.5}{0.5}=1 and ω=4=2\omega = \sqrt{4} = 2 rad/s. Check: s3+0.5s2+4s+2=(s2+4)(s+0.5)s^3+0.5s^2+4s+2 = (s^2+4)(s+0.5), which has roots ±j2\pm j2.

  • 2081 Bhadra · 6 marks

A unity feedback system has the feedforward transfer function G(s) = K(s+13)/[s(s+3)(s+7)]. Using R-H Criterion, find the range of K for the system to be stable. When does the system just oscillate and what would be that frequency during sustained oscillation?

Answer

The closed-loop characteristic equation 1+G(s)=01+G(s)=0 is tested with the Routh array. The system just oscillates (is marginally stable) when the s1s^1 row becomes zero.

Characteristic equation

s(s+3)(s+7)+K(s+13)=0s3+10s2+(21+K)s+13K=0\begin{aligned} s(s+3)(s+7) + K(s+13) &= 0 \\ s^3 + 10s^2 + (21+K)s + 13K &= 0 \end{aligned}

Routh array

RowCol 1Col 2
s3s^3121+K21+K
s2s^21013K13K
s1s^110(21+K)−13K10=210−3K10\frac{10(21+K)-13K}{10}=\frac{210-3K}{10}0
s0s^013K13K

Range of K

  • s1s^1 row: 210−3K>0⇒K<70210-3K>0 \Rightarrow K<70
  • s0s^0 row: 13K>0⇒K>013K>0 \Rightarrow K>0
0<K<700 < K < 70

Sustained oscillation

At K=70K = 70 the s1s^1 row is zero, so the system just oscillates. Auxiliary equation from the s2s^2 row:

10s2+13K=010s2+910=0s2=−91⇒s=±j9.54\begin{aligned} 10s^2 + 13K &= 0 \\ 10s^2 + 910 &= 0 \\ s^2 &= -91 \Rightarrow s = \pm j9.54 \end{aligned}

Answer: stable for 0<K<700<K<70; it just oscillates at K=70K=70, with frequency ω=91=9.54\omega=\sqrt{91}=9.54 rad/s.

  • 2081 Baisakh · 6 marks

Using Routh-Hurwitz criterion determine the relation between "K" and "T" so that unity feedback control system whose open loop transfer function given below is stable. G(s) = K/(s[s(s+10) + T])

Answer

For unity feedback, the characteristic equation is 1+G(s)=01+G(s)=0. All first-column Routh elements must be positive.

Characteristic equation

s[s(s+10)+T]+K=0s3+10s2+Ts+K=0\begin{aligned} s[s(s+10)+T] + K &= 0 \\ s^3 + 10s^2 + Ts + K &= 0 \end{aligned}

Routh array

RowCol 1Col 2
s3s^31TT
s2s^210KK
s1s^110T−K10\frac{10T-K}{10}0
s0s^0KK

Conditions

  • s0s^0 row: K>0K > 0
  • s1s^1 row: 10T−K>0⇒K<10T10T - K > 0 \Rightarrow K < 10T
  • From these, T>0T > 0 (also needed so that all coefficients are positive).
0<K<10T0 < K < 10T

Interpretation: for a given TT, the gain can be raised up to 10T10T. At K=10TK = 10T the system is marginally stable and oscillates at ω=K/10=T\omega = \sqrt{K/10} = \sqrt{T} rad/s (from 10s2+K=010s^2+K=0). For example, with T=5T = 5 the system is stable for 0<K<500<K<50.

Answer: relation for stability: 0<K<10T0 < K < 10T (with T>0T>0).

  • 2080 Bhadra · 6 marks

For a unity feedback system having open loop transfer function G(s) = k/[s(1+Ts)], determine the values of K and T if it is desired that all the roots of closed loop system should lie in the region towards the left of s = −a.

Answer

To make all roots lie to the left of s=−as=-a, shift the imaginary axis to s=−as=-a by putting s=z−as = z - a. Then apply the Routh criterion to the new polynomial in zz (relative stability).

Characteristic equation

1+Ks(1+Ts)=0Ts2+s+K=0\begin{aligned} 1 + \frac{K}{s(1+Ts)} &= 0 \\ Ts^2 + s + K &= 0 \end{aligned}

Shift the axis: s=z−as = z - a

T(z−a)2+(z−a)+K=0Tz2+(1−2aT)z+(Ta2−a+K)=0\begin{aligned} T(z-a)^2 + (z-a) + K &= 0 \\ Tz^2 + (1-2aT)z + (Ta^2 - a + K) &= 0 \end{aligned}

Routh array in z

RowCol 1Col 2
z2z^2TTTa2−a+KTa^2-a+K
z1z^11−2aT1-2aT0
z0z^0Ta2−a+KTa^2-a+K

For no sign change (all roots left of z=0z=0, i.e. left of s=−as=-a):

  1. T>0T > 0
  2. 1−2aT>0⇒T<12a1-2aT > 0 \Rightarrow T < \dfrac{1}{2a}
  3. Ta2−a+K>0⇒K>a−a2T=a(1−aT)Ta^2 - a + K > 0 \Rightarrow K > a - a^2T = a(1-aT)
0<T<12a,K>a(1−aT)0 < T < \frac{1}{2a}, \qquad K > a(1-aT)

Physical meaning: the sum of the closed-loop roots is −1T-\frac{1}{T}, so both roots can be left of −a-a only if 1T>2a\frac{1}{T} > 2a. The gain must be large enough that the slower real root moves past −a-a.

Example: for a=1a=1 and T=0.25T=0.25: K>1(1−0.25)=0.75K > 1(1-0.25)=0.75. With K=1K=1, 0.25s2+s+1=00.25s^2+s+1=0 gives s=−2,−2s = -2, -2, both left of −1-1.

  • 2080 Baisakh · 6 marks

Check stability of the system as given below in block diagram. [Figure: unity negative feedback system with forward path G(s) = 56/[s(s⁴ + 7s³ + 6s² + 42s + 8)]]

Answer

Result: the system is marginally stable. It has roots at ±j2\pm j\sqrt2 and ±j2\pm j2, one root at s=−7s=-7, and none in the RHP.

For unity negative feedback, the characteristic equation is 1+G(s)=01+G(s)=0. Its Routh array is formed and the first column is examined.

Characteristic equation

s(s4+7s3+6s2+42s+8)+56=0s5+7s4+6s3+42s2+8s+56=0\begin{aligned} s(s^4+7s^3+6s^2+42s+8) + 56 &= 0 \\ s^5 + 7s^4 + 6s^3 + 42s^2 + 8s + 56 &= 0 \end{aligned}

Routh array

RowCol 1Col 2Col 3
s5s^5168
s4s^474256
s3s^37(6)−427=0\frac{7(6)-42}{7}=07(8)−567=0\frac{7(8)-56}{7}=0

The s3s^3 row is all zeros. Auxiliary equation from the s4s^4 row:

A(s)=7s4+42s2+56,dAds=28s3+84sA(s) = 7s^4 + 42s^2 + 56, \qquad \frac{dA}{ds} = 28s^3 + 84s
RowCol 1Col 2
s3s^32884
s2s^228(42)−7(84)28=21\frac{28(42)-7(84)}{28}=2156
s1s^121(84)−28(56)21=9.33\frac{21(84)-28(56)}{21}=9.33
s0s^056

First column: 1, 7, 28, 21, 9.33, 561,\ 7,\ 28,\ 21,\ 9.33,\ 56. No sign change, so no root is in the RHP.

Roots on the imaginary axis

7s4+42s2+56=7(s2+2)(s2+4)=0⇒s=±j1.414, ±j27s^4+42s^2+56 = 7(s^2+2)(s^2+4) = 0 \Rightarrow s = \pm j1.414,\ \pm j2

The fifth root: q(s)(s2+2)(s2+4)=s+7\frac{q(s)}{(s^2+2)(s^2+4)} = s+7, so s=−7s=-7.

RegionRoots
RHPnone
jωj\omega axis±j1.414\pm j1.414, ±j2\pm j2 (non-repeated)
LHP−7-7

Conclusion

The poles on the jωj\omega axis are simple (non-repeated), and none are in the RHP. The system is marginally stable: its response contains sustained oscillations at 1.414 rad/s and 2 rad/s.

  • 2078 Bhadra · 6 marks

Use RH criterion to determine number of roots on right side, left side and on the imaginary axis itself of s-plane for the system below. [Figure: unity negative feedback system with forward path G(s) = 200/[s(s³ + 6s² + 11s + 6)]]

Answer

Result: RHP = 2, LHP = 2, jωj\omega axis = 0. The system is unstable.

For unity negative feedback the characteristic equation is 1+G(s)=01+G(s)=0. The number of sign changes in the first column of the Routh array gives the number of roots in the right half plane.

Characteristic equation

s(s3+6s2+11s+6)+200=0s4+6s3+11s2+6s+200=0\begin{aligned} s(s^3+6s^2+11s+6) + 200 &= 0 \\ s^4 + 6s^3 + 11s^2 + 6s + 200 &= 0 \end{aligned}

Routh array

RowCol 1Col 2Col 3
s4s^4111200
s3s^3660
s2s^26(11)−1(6)6=10\frac{6(11)-1(6)}{6}=106(200)−06=200\frac{6(200)-0}{6}=200
s1s^110(6)−6(200)10=−114\frac{10(6)-6(200)}{10}=-1140
s0s^0200

First column: 1, 6, 10, −114, 2001,\ 6,\ 10,\ -114,\ 200.

Sign changes: +10→−114+10 \to -114 (one) and −114→+200-114 \to +200 (two), so there are 2 sign changes.

Root location

RegionNumber of roots
Right half s-plane2
Left half s-plane4−2=24-2 = 2
On jωj\omega axis0 (no zero row)

The numerical roots (s≈1.28±j2.54s \approx 1.28 \pm j2.54 and s≈−4.28±j2.54s \approx -4.28 \pm j2.54) agree with this.

Answer: 2 roots in the RHP, 2 in the LHP, none on the imaginary axis. The closed-loop system is unstable; the gain of 200 is too high.

  • 2076 Chaitra · 6 marks

In the following system, determine K (and a) if the system just oscillates at a frequency 2 rad/sec. [Figure: unity negative feedback system with forward path G(s) = k(s+1)/(s³ + as² + 2s + 1)]

Answer

A system "just oscillates" when it is marginally stable. In the Routh array, the s1s^1 row then becomes zero, and the auxiliary equation from the s2s^2 row gives the frequency of oscillation.

Characteristic equation

1+K(s+1)s3+as2+2s+1=0s3+as2+(2+K)s+(1+K)=0\begin{aligned} 1 + \frac{K(s+1)}{s^3+as^2+2s+1} &= 0 \\ s^3 + as^2 + (2+K)s + (1+K) &= 0 \end{aligned}

Routh array

RowCol 1Col 2
s3s^312+K2+K
s2s^2aa1+K1+K
s1s^1a(2+K)−(1+K)a\frac{a(2+K)-(1+K)}{a}0
s0s^01+K1+K

Condition for sustained oscillation

s1s^1 row =0=0:

a(2+K)=1+K...(1)a(2+K) = 1+K \qquad \text{...(1)}

Auxiliary equation from the s2s^2 row, with s=jωs = j\omega:

as2+(1+K)=0ω2=1+Ka...(2)\begin{aligned} as^2 + (1+K) &= 0 \\ \omega^2 &= \frac{1+K}{a} \qquad \text{...(2)} \end{aligned}

From (1), 1+Ka=2+K\frac{1+K}{a} = 2+K, so (2) becomes ω2=2+K\omega^2 = 2+K.

Substitute ω=2\omega = 2 rad/s

4=2+K⇒K=2a=1+K2+K=34=0.75\begin{aligned} 4 &= 2+K \Rightarrow K = 2 \\ a &= \frac{1+K}{2+K} = \frac{3}{4} = 0.75 \end{aligned}

Check

With K=2K=2, a=0.75a=0.75: s3+0.75s2+4s+3=(s2+4)(s+0.75)s^3+0.75s^2+4s+3 = (s^2+4)(s+0.75). The roots are ±j2\pm j2 and −0.75-0.75, so the system oscillates at 2 rad/s.

Answer: K=2K = 2, a=0.75a = 0.75.

  • 2076 Chaitra · 2 marks

How does the location of poles affect the stability in control system?

Answer

The stability of a system depends only on where the poles of its closed-loop transfer function (the roots of the characteristic equation) lie in the s-plane. Each pole s=σ±jωs = \sigma \pm j\omega adds a term eσtsin⁡(ωt)e^{\sigma t}\sin(\omega t) to the response.

Pole locationResponse termStability
Left half plane (σ<0\sigma<0)Decays to zeroStable
Simple poles on jωj\omega axisConstant or steady oscillationMarginally stable
Repeated poles on jωj\omega axistsin⁡ωtt\sin\omega t, growsUnstable
Right half plane (σ>0\sigma>0)Grows exponentiallyUnstable
  • The further left the poles are, the faster the response decays. This means greater relative stability.
  • Poles close to the jωj\omega axis (dominant poles) decay slowly and decide the transient response.
  • Imaginary part ω\omega sets the frequency of oscillation; real poles give no oscillation.
  • 2076 Asoj · 4 marks

Check stability for the system with open loop transfer function G(s)H(s) = 2/(2s⁵ + 3s⁴ + 2s³ + s² + 2s) using R-H criterion.

Answer

Result: 2 sign changes, so the closed-loop system has 2 roots in the RHP and is unstable.

The closed-loop stability is decided by the characteristic equation 1+G(s)H(s)=01+G(s)H(s)=0.

2s5+3s4+2s3+s2+2s+2=0\begin{aligned} 2s^5+3s^4+2s^3+s^2+2s + 2 &= 0 \end{aligned}

Routh array

RowCol 1Col 2Col 3
s5s^5222
s4s^4312
s3s^33(2)−2(1)3=43\frac{3(2)-2(1)}{3}=\frac{4}{3}3(2)−2(2)3=23\frac{3(2)-2(2)}{3}=\frac{2}{3}0
s2s^243(1)−3⋅2343=−0.5\frac{\frac43(1)-3\cdot\frac23}{\frac43}=-0.543(2)−043=2\frac{\frac43(2)-0}{\frac43}=2
s1s^1−0.5⋅23−43(2)−0.5=6\frac{-0.5\cdot\frac23-\frac43(2)}{-0.5}=60
s0s^02

First column: 2, 3, 1.33, −0.5, 6, 22,\ 3,\ 1.33,\ -0.5,\ 6,\ 2.

There are 2 sign changes (1.33→−0.51.33 \to -0.5 and −0.5→6-0.5 \to 6), so 2 closed-loop poles lie in the right half s-plane.

Answer: the closed-loop system is unstable, with 2 poles in the RHP and 3 in the LHP. The roots are approximately 0.51±j0.750.51\pm j0.75, −0.76±j0.80-0.76\pm j0.80 and −1-1.

  • 2075 Chaitra · 6 marks

Using R-H criteria find the range of K for system having characteristic equation shown below, to be stable. s⁴ + 2s³ + (4+K)s² + 9s + 25 = 0

Answer

Form the Routh array with KK and make every first-column element positive.

s4+2s3+(4+K)s2+9s+25=0s^4 + 2s^3 + (4+K)s^2 + 9s + 25 = 0

Routh array

RowCol 1Col 2Col 3
s4s^414+K4+K25
s3s^3290
s2s^22(4+K)−92=2K−12\frac{2(4+K)-9}{2}=\frac{2K-1}{2}25
s1s^12K−12(9)−2(25)2K−12=18K−1092K−1\frac{\frac{2K-1}{2}(9)-2(25)}{\frac{2K-1}{2}}=\frac{18K-109}{2K-1}0
s0s^025

Conditions

  1. s2s^2 row: 2K−12>0⇒K>0.5\frac{2K-1}{2}>0 \Rightarrow K>0.5
  2. s1s^1 row: with 2K−1>02K-1>0, we need 18K−109>0⇒K>10918=6.05618K-109>0 \Rightarrow K > \frac{109}{18} = 6.056
  3. s0s^0 row: 25>025>0 always true.

Condition 2 is stricter, so:

K>6.056K > 6.056

Marginal value

At K=109/18=6.056K = 109/18 = 6.056, the s1s^1 row is zero. The auxiliary equation 509s2+25=0\frac{50}{9}s^2 + 25 = 0 gives s=±j2.12s = \pm j2.12, so the system would oscillate at 2.12 rad/s.

Answer: the system is stable for K>6.056K > 6.056 (i.e. K>109/18K>109/18). There is no upper limit.

  • 2073 Shrawan · 4 marks

For a closed loop system presented by the block diagram below, determine the range of controller gain (Kp, KI) so that the PI controller provides the stable output. [Figure: R → summing point (+, −) → PI controller (Kp + KI/s) → plant 1/[(s+1)(s+2)] → y; unity negative feedback from y]

Answer

The PI controller Kp+KIsK_p + \frac{K_I}{s} adds a pole at the origin. Find the closed-loop characteristic equation and apply Routh's criterion.

Characteristic equation

G(s)=(Kp+KIs)1(s+1)(s+2)=Kps+KIs(s+1)(s+2)1+G(s)=0⇒s(s2+3s+2)+Kps+KI=0⇒s3+3s2+(2+Kp)s+KI=0\begin{aligned} G(s) &= \left(K_p + \frac{K_I}{s}\right)\frac{1}{(s+1)(s+2)} = \frac{K_ps + K_I}{s(s+1)(s+2)} \\ 1+G(s) = 0 &\Rightarrow s(s^2+3s+2) + K_ps + K_I = 0 \\ &\Rightarrow s^3 + 3s^2 + (2+K_p)s + K_I = 0 \end{aligned}

Routh array

RowCol 1Col 2
s3s^312+Kp2+K_p
s2s^23KIK_I
s1s^13(2+Kp)−KI3\frac{3(2+K_p)-K_I}{3}0
s0s^0KIK_I

Conditions for stability

  • s0s^0 row: KI>0K_I > 0
  • s1s^1 row: 3(2+Kp)−KI>0⇒KI<3(Kp+2)3(2+K_p) - K_I > 0 \Rightarrow K_I < 3(K_p+2)
  • This also requires Kp>−2K_p > -2.
0<KI<3(Kp+2)0 < K_I < 3(K_p + 2)

Example: with Kp=1K_p = 1, the integral gain must satisfy 0<KI<90 < K_I < 9; with Kp=4K_p = 4, 0<KI<180 < K_I < 18. A larger KpK_p allows a larger KIK_I.

  • 2072 Chaitra · 4 marks

Find the range of 'K' for stable operation using R-H criteria. [Figure: R(s) → summing point (+, −) → K → 1/[s(s²+s+1)(s+2)] → C(s); unity negative feedback]

Answer

For unity feedback, the characteristic equation is 1+G(s)=01+G(s)=0, with G(s)=Ks(s2+s+1)(s+2)G(s)=\frac{K}{s(s^2+s+1)(s+2)}.

Characteristic equation

s(s2+s+1)(s+2)+K=0s4+3s3+3s2+2s+K=0\begin{aligned} s(s^2+s+1)(s+2) + K &= 0 \\ s^4 + 3s^3 + 3s^2 + 2s + K &= 0 \end{aligned}

Routh array

RowCol 1Col 2Col 3
s4s^413KK
s3s^3320
s2s^23(3)−1(2)3=73\frac{3(3)-1(2)}{3}=\frac{7}{3}KK
s1s^173(2)−3K73=2−9K7\frac{\frac73(2)-3K}{\frac73}=2-\frac{9K}{7}0
s0s^0KK

Conditions

  • s1s^1 row: 2−9K7>0⇒K<149=1.5562 - \frac{9K}{7} > 0 \Rightarrow K < \frac{14}{9} = 1.556
  • s0s^0 row: K>0K > 0
0<K<1.5560 < K < 1.556

At K=14/9K = 14/9 the system is marginally stable. The auxiliary equation 73s2+149=0\frac73 s^2 + \frac{14}{9} = 0 gives ω=2/3=0.816\omega = \sqrt{2/3} = 0.816 rad/s.

Answer: stable for 0<K<1490 < K < \frac{14}{9} (= 1.556).

  • 2072 Chaitra · 6 marks

Determine value of 'K' and 'b' so that the unity feedback system with open loop transfer function G(s) = K(s+1)/(s³ + bs² + 3s + 1) [rest of the question is not printed in the paper].

Answer

Result (assuming oscillation at 2 rad/s): K=1K = 1, b=0.5b = 0.5. In general, K=3b−11−bK = \frac{3b-1}{1-b} and ω=21−b\omega=\sqrt{\frac{2}{1-b}}.

Assumption: the end of the question is missing. It is taken in its usual form: "...so that the system oscillates at a frequency of 2 rad/s". The general relations are also derived, so any other given frequency can be substituted.

Characteristic equation

s3+bs2+3s+1+K(s+1)=0s3+bs2+(3+K)s+(1+K)=0\begin{aligned} s^3+bs^2+3s+1 + K(s+1) &= 0 \\ s^3 + bs^2 + (3+K)s + (1+K) &= 0 \end{aligned}

Routh array

RowCol 1Col 2
s3s^313+K3+K
s2s^2bb1+K1+K
s1s^1b(3+K)−(1+K)b\frac{b(3+K)-(1+K)}{b}0
s0s^01+K1+K

Conditions for sustained oscillation

The s1s^1 row must be zero:

b(3+K)=1+K...(1)b(3+K) = 1+K \qquad \text{...(1)}

Auxiliary equation (from the s2s^2 row) with s=jωs=j\omega:

bs2+(1+K)=0⇒ω2=1+Kb...(2)bs^2 + (1+K) = 0 \Rightarrow \omega^2 = \frac{1+K}{b} \qquad \text{...(2)}

From (1) and (2): ω2=3+K\omega^2 = 3 + K.

Substitute ω=2\omega = 2 rad/s

4=3+K⇒K=1b=1+Kω2=24=0.5\begin{aligned} 4 &= 3 + K \Rightarrow K = 1 \\ b &= \frac{1+K}{\omega^2} = \frac{2}{4} = 0.5 \end{aligned}

Check: s3+0.5s2+4s+2=(s2+4)(s+0.5)s^3+0.5s^2+4s+2 = (s^2+4)(s+0.5). The roots are ±j2\pm j2 and −0.5-0.5, so the system oscillates at 2 rad/s.

Answer: K=1K = 1, b=0.5b = 0.5. In general: K=3b−11−bK = \frac{3b-1}{1-b} and ω=21−b\omega = \sqrt{\frac{2}{1-b}}. The system is stable when b(3+K)>1+Kb(3+K) > 1+K.

  • 2071 Shrawan · 6 marks

Using R-H criteria, tell how many roots of polynomial are in right half s-plane, in left half s-plane and on jω axis. s⁶ + 2s⁵ + 8s⁴ + 12s³ + 20s² + 16s + 16 = 0

Answer

Result: RHP = 0, LHP = 2, jωj\omega axis = 4. The system is marginally stable.

By the Routh–Hurwitz criterion, the number of sign changes in the first column equals the number of RHP roots. A zero row shows roots symmetric about the origin, which are found from the auxiliary equation.

s6+2s5+8s4+12s3+20s2+16s+16=0s^6 + 2s^5 + 8s^4 + 12s^3 + 20s^2 + 16s + 16 = 0

Routh array

RowCol 1Col 2Col 3Col 4
s6s^6182016
s5s^5212160
s4s^42(8)−1(12)2=2\frac{2(8)-1(12)}{2}=22(20)−1(16)2=12\frac{2(20)-1(16)}{2}=1216
s3s^32(12)−2(12)2=0\frac{2(12)-2(12)}{2}=02(16)−2(16)2=0\frac{2(16)-2(16)}{2}=0

The s3s^3 row is all zeros, so there are roots placed symmetrically about the origin. Auxiliary equation from the s4s^4 row:

A(s)=2s4+12s2+16,dAds=8s3+24sA(s) = 2s^4 + 12s^2 + 16, \qquad \frac{dA}{ds} = 8s^3 + 24s
RowCol 1Col 2
s3s^3824
s2s^28(12)−2(24)8=6\frac{8(12)-2(24)}{8}=68(16)−08=16\frac{8(16)-0}{8}=16
s1s^16(24)−8(16)6=2.67\frac{6(24)-8(16)}{6}=2.670
s0s^016

First column: 1, 2, 2, 8, 6, 2.67, 161,\ 2,\ 2,\ 8,\ 6,\ 2.67,\ 16. No sign change, so no root is in the RHP.

Roots of the auxiliary equation

2s4+12s2+16=2(s2+2)(s2+4)=0s=±j1.414, ±j2\begin{aligned} 2s^4+12s^2+16 &= 2(s^2+2)(s^2+4) = 0 \\ s &= \pm j1.414,\ \pm j2 \end{aligned}

These four roots lie on the jωj\omega axis and are not repeated. The other factor is

s6+2s5+8s4+12s3+20s2+16s+16(s2+2)(s2+4)=s2+2s+2  ⇒  s=−1±j1\frac{s^6+2s^5+8s^4+12s^3+20s^2+16s+16}{(s^2+2)(s^2+4)} = s^2+2s+2 \;\Rightarrow\; s = -1\pm j1
RegionNumberRoots
Right half plane0none
jωj\omega axis4±j1.414\pm j1.414, ±j2\pm j2
Left half plane2−1±j1-1\pm j1

The jωj\omega-axis roots are simple, so the system is marginally stable: it oscillates at 1.414 rad/s and 2 rad/s.

  • 2070 Chaitra (old course) · 8 marks

Check the stability of the system represented by the following characteristic equation using R-H criteria: s⁴ + 8s³ + 18s² + 16s + 50 = 0

Answer

Result: the system is unstable, with 2 roots in the right half plane.

The Routh–Hurwitz criterion says a system is stable only if all elements in the first column of the Routh array have the same sign. The number of sign changes equals the number of roots in the right half s-plane.

s4+8s3+18s2+16s+50=0s^4 + 8s^3 + 18s^2 + 16s + 50 = 0

Necessary condition: all coefficients are present and positive, so it is satisfied. This alone does not prove stability, so the array is needed.

Routh array

RowCol 1Col 2Col 3
s4s^411850
s3s^38160
s2s^28(18)−1(16)8=16\frac{8(18)-1(16)}{8}=168(50)−1(0)8=50\frac{8(50)-1(0)}{8}=50
s1s^116(16)−8(50)16=−9\frac{16(16)-8(50)}{16}=-90
s0s^050

Examination of the first column

First column: 1, 8, 16, −9, 501,\ 8,\ 16,\ -9,\ 50

  • +16→−9+16 \to -9: first sign change
  • −9→+50-9 \to +50: second sign change

2 sign changes, so 2 roots lie in the right half of the s-plane.

RegionNumber of roots
Right half plane2
Left half plane2
jωj\omega axis0

The actual roots are s≈0.185±j1.64s \approx 0.185 \pm j1.64 and s≈−4.18±j0.93s \approx -4.18 \pm j0.93, which agrees with the Routh result.

Answer: the system is unstable. It has two roots in the RHP, so its response grows as an oscillation with an increasing envelope.

  • 2070 Chaitra · 8 marks

The open loop transfer function of a closed loop system is G(s) = K(s+1)/[s(s+2)(s+3)]; find maximum possible K for which the poles lie on left of point −0.5.

Answer

Result: all poles lie left of s=−0.5s=-0.5 when K>3.75K > 3.75. There is no finite maximum; K=3.75K = 3.75 is the limiting value.

To check that all poles lie to the left of s=−0.5s=-0.5, shift the imaginary axis to s=−0.5s=-0.5 by putting s=z−0.5s = z - 0.5. Then apply the Routh criterion in zz. Unity feedback is assumed.

Characteristic equation

s(s+2)(s+3)+K(s+1)=0s3+5s2+(6+K)s+K=0\begin{aligned} s(s+2)(s+3) + K(s+1) &= 0 \\ s^3 + 5s^2 + (6+K)s + K &= 0 \end{aligned}

Shift: s=z−0.5s = z - 0.5

(z−0.5)(z+1.5)(z+2.5)=z3+3.5z2+1.75z−1.875K(z−0.5+1)=Kz+0.5K\begin{aligned} (z-0.5)(z+1.5)(z+2.5) &= z^3 + 3.5z^2 + 1.75z - 1.875 \\ K(z-0.5+1) &= Kz + 0.5K \end{aligned} z3+3.5z2+(1.75+K)z+(0.5K−1.875)=0z^3 + 3.5z^2 + (1.75+K)z + (0.5K - 1.875) = 0

Routh array in z

RowCol 1Col 2
z3z^311.75+K1.75+K
z2z^23.50.5K−1.8750.5K-1.875
z1z^13.5(1.75+K)−(0.5K−1.875)3.5=3K+83.5\frac{3.5(1.75+K)-(0.5K-1.875)}{3.5}=\frac{3K+8}{3.5}0
z0z^00.5K−1.8750.5K-1.875

Conditions

  • z1z^1 row: 3K+8>0⇒K>−2.673K + 8 > 0 \Rightarrow K > -2.67 (true for K>0K>0)
  • z0z^0 row: 0.5K−1.875>0⇒K>3.750.5K - 1.875 > 0 \Rightarrow K > 3.75

So all closed-loop poles lie to the left of s=−0.5s=-0.5 when

K>3.75K > 3.75

Comment on "maximum K"

For this system there is no finite maximum. As K→∞K\to\infty, one pole moves to the zero at −1-1, and the other two follow asymptotes at ±90∘\pm90^\circ from the centroid (0−2−3)−(−1)2=−2\frac{(0-2-3)-(-1)}{2}=-2, which is left of −0.5-0.5. The limiting (boundary) value is K=3.75K=3.75. At K=3.75K=3.75 the poles are s=−0.5s=-0.5 and s=−2.25±j1.56s=-2.25\pm j1.56, so one pole is exactly at −0.5-0.5.

Answer: all poles lie left of s=−0.5s=-0.5 for K>3.75K > 3.75; the boundary value is K=3.75K = 3.75.

  • 2068 Chaitra · 8 marks

Apply RH criteria to determine the range of 'K' for which a unity feedback system with G(s) = K(s+13)/[s(s+3)(s+7)] will be stable.

Answer

For unity feedback, the closed-loop characteristic equation is 1+G(s)=01+G(s)=0. The system is stable when the first column of the Routh array has no sign change.

Characteristic equation

1+K(s+13)s(s+3)(s+7)=0s(s2+10s+21)+Ks+13K=0s3+10s2+(21+K)s+13K=0\begin{aligned} 1 + \frac{K(s+13)}{s(s+3)(s+7)} &= 0 \\ s(s^2+10s+21) + Ks + 13K &= 0 \\ s^3 + 10s^2 + (21+K)s + 13K &= 0 \end{aligned}

Routh array

RowCol 1Col 2
s3s^3121+K21+K
s2s^21013K13K
s1s^110(21+K)−1(13K)10=210−3K10\frac{10(21+K)-1(13K)}{10}=\frac{210-3K}{10}0
s0s^013K13K

Conditions for stability

  1. From the s1s^1 row: 210−3K10>0⇒K<70\frac{210-3K}{10} > 0 \Rightarrow K < 70
  2. From the s0s^0 row: 13K>0⇒K>013K > 0 \Rightarrow K > 0
0<K<700 < K < 70

Marginal stability

At K=70K = 70 the s1s^1 row vanishes. Auxiliary equation:

10s2+13(70)=0⇒s2=−91⇒s=±j9.5410s^2 + 13(70) = 0 \Rightarrow s^2 = -91 \Rightarrow s = \pm j9.54

So at K=70K=70 the system oscillates at 9.54 rad/s, and for K>70K>70 two poles move into the RHP.

Answer: the system is stable for 0<K<700 < K < 70.

  • 2068 Baisakh (old course) · 8 marks

The open loop TF of a unity feedback control system is given as G(s) = K/[(s+2)(s+4)(s²+6s+25)]. Determine the range of gain K for the system to be stable. Also determine the value of K which will cause the sustained oscillation and corresponding oscillation frequency.

Answer

Write the closed-loop characteristic equation 1+G(s)=01+G(s)=0 and apply the Routh criterion. Sustained oscillation occurs when the s1s^1 row becomes zero, and the auxiliary equation from the s2s^2 row gives the frequency.

Characteristic equation

(s+2)(s+4)(s2+6s+25)+K=0(s2+6s+8)(s2+6s+25)+K=0s4+12s3+69s2+198s+(200+K)=0\begin{aligned} (s+2)(s+4)(s^2+6s+25) + K &= 0 \\ (s^2+6s+8)(s^2+6s+25) + K &= 0 \\ s^4 + 12s^3 + 69s^2 + 198s + (200+K) &= 0 \end{aligned}

Routh array

RowCol 1Col 2Col 3
s4s^4169200+K200+K
s3s^3121980
s2s^212(69)−19812=52.5\frac{12(69)-198}{12}=52.5200+K200+K
s1s^152.5(198)−12(200+K)52.5=7995−12K52.5\frac{52.5(198)-12(200+K)}{52.5}=\frac{7995-12K}{52.5}0
s0s^0200+K200+K

Range of K

  • s1s^1 row: 7995−12K>0⇒K<666.257995 - 12K > 0 \Rightarrow K < 666.25
  • s0s^0 row: 200+K>0⇒K>−200200 + K > 0 \Rightarrow K > -200
−200<K<666.25(for positive gain: 0<K<666.25)-200 < K < 666.25 \qquad (\text{for positive gain: } 0 < K < 666.25)

Value of K for sustained oscillation

Kmar=799512=666.25K_{mar} = \frac{7995}{12} = 666.25

Frequency of oscillation

Auxiliary equation from the s2s^2 row:

52.5s2+(200+666.25)=0s2=−866.2552.5=−16.5ω=16.5=4.062 rad/s\begin{aligned} 52.5s^2 + (200 + 666.25) &= 0 \\ s^2 &= -\frac{866.25}{52.5} = -16.5 \\ \omega &= \sqrt{16.5} = 4.062\ \text{rad/s} \end{aligned}

Check: with K=666.25K = 666.25 the roots are ±j4.062\pm j4.062 and −6±j4.062-6 \pm j4.062.

Answer: stable for 0<K<666.250 < K < 666.25; sustained oscillation at K=666.25K = 666.25 with ω=4.06\omega = 4.06 rad/s.

  • 2066 Bhadra (old course) · 8 marks

Using R-H criteria, tell how many roots of polynomial are in right half plane, in left half plane and on jω-axis. P(s) = s⁵ + 3s⁴ + 5s³ + 4s² + s + 3.

Answer

Result: RHP = 2, LHP = 3, jωj\omega axis = 0. The system is unstable.

Routh–Hurwitz criterion: the number of sign changes in the first column of the Routh array equals the number of roots in the right half plane. A complete zero row would indicate roots on the jωj\omega axis.

P(s)=s5+3s4+5s3+4s2+s+3P(s) = s^5 + 3s^4 + 5s^3 + 4s^2 + s + 3

Routh array

RowCol 1Col 2Col 3
s5s^5151
s4s^4343
s3s^33(5)−1(4)3=113\frac{3(5)-1(4)}{3}=\frac{11}{3}3(1)−1(3)3=0\frac{3(1)-1(3)}{3}=0
s2s^2113(4)−3(0)113=4\frac{\frac{11}{3}(4)-3(0)}{\frac{11}{3}}=4113(3)−0113=3\frac{\frac{11}{3}(3)-0}{\frac{11}{3}}=3
s1s^14(0)−113(3)4=−114\frac{4(0)-\frac{11}{3}(3)}{4}=-\frac{11}{4}0
s0s^03

First column: 1, 3, 3.67, 4, −2.75, 31,\ 3,\ 3.67,\ 4,\ -2.75,\ 3.

  • 4→−2.754 \to -2.75: one sign change
  • −2.75→3-2.75 \to 3: second sign change

Root distribution

No row became entirely zero, so no root lies on the jωj\omega axis.

RegionNumber of roots
Right half plane2
jωj\omega axis0
Left half plane5−2=35 - 2 = 3

The roots (≈0.256±j0.720\approx 0.256\pm j0.720, −0.941±j1.504-0.941\pm j1.504, −1.631-1.631) confirm this.

Answer: 2 roots in the RHP, 3 in the LHP, none on the jωj\omega axis. The system is unstable.

  • 2066 Jestha (old course) · 6 marks

For a process control system shown below, find the range of K for which the roots of characteristic equation are more negative than s = −2. [Figure: unity negative feedback system with forward path K(s+10)/[s(s+3)]]

Answer

"Roots more negative than s=−2s=-2" means all closed-loop poles must lie to the left of the line s=−2s=-2. Shift the imaginary axis by putting s=z−2s = z - 2, then apply the Routh criterion in zz.

Characteristic equation

1+K(s+10)s(s+3)=0s2+(3+K)s+10K=0\begin{aligned} 1 + \frac{K(s+10)}{s(s+3)} &= 0 \\ s^2 + (3+K)s + 10K &= 0 \end{aligned}

Shift the axis: s=z−2s = z - 2

(z−2)2+(3+K)(z−2)+10K=0z2−4z+4+(3+K)z−6−2K+10K=0z2+(K−1)z+(8K−2)=0\begin{aligned} (z-2)^2 + (3+K)(z-2) + 10K &= 0 \\ z^2 - 4z + 4 + (3+K)z - 6 - 2K + 10K &= 0 \\ z^2 + (K-1)z + (8K-2) &= 0 \end{aligned}

Routh array in z

RowCol 1Col 2
z2z^218K−28K-2
z1z^1K−1K-10
z0z^08K−28K-2

Conditions

  • z1z^1 row: K−1>0⇒K>1K - 1 > 0 \Rightarrow K > 1
  • z0z^0 row: 8K−2>0⇒K>0.258K - 2 > 0 \Rightarrow K > 0.25

Both must hold, so

K>1K > 1

Check: at K=1K = 1, s2+4s+10=0s^2 + 4s + 10 = 0 gives s=−2±j2.45s = -2 \pm j2.45, exactly on the line s=−2s=-2. For K>1K>1 the real part of the roots (or both real roots) is more negative than −2-2.

Answer: all roots are more negative than s=−2s = -2 for K>1K > 1.

  • 2081 Bhadra · 3+5 marks

What is relative and absolute stability? Check the stability of system with characteristic equation: s⁵ + s⁴ + 2s³ + 2s² + 3s + 5 = 0 using R-H criteria.

Answer

Absolute and relative stability

  • Absolute stability answers yes or no: is the system stable or not? A system is absolutely stable if all closed-loop poles lie in the left half of the s-plane, so every bounded input gives a bounded output and the natural response decays to zero. The Routh–Hurwitz criterion checks absolute stability.
  • Relative stability measures how stable a stable system is, i.e. how far its poles are from the jωj\omega axis (instability boundary). Poles further left decay faster and give less oscillation. It is measured by the real part of the dominant poles (settling time), damping ratio, or in the frequency domain by gain margin and phase margin. In Routh's method, it is found by shifting the axis (s=z−σs = z - \sigma) and testing again.
Absolute stabilityRelative stability
Stable or unstable (qualitative)Degree of stability (quantitative)
Checks sign of real parts of polesChecks distance of poles from jωj\omega axis
Routh–Hurwitz, pole locationShifted Routh, GM, PM, damping ratio

Stability of s5+s4+2s3+2s2+3s+5=0s^5 + s^4 + 2s^3 + 2s^2 + 3s + 5 = 0

RowCol 1Col 2Col 3
s5s^5123
s4s^4125
s3s^31(2)−1(2)1=0→ε\frac{1(2)-1(2)}{1}=0 \to \varepsilon1(3)−1(5)1=−2\frac{1(3)-1(5)}{1}=-2
s2s^22ε+2ε\frac{2\varepsilon+2}{\varepsilon}5
s1s^1−2−5ε22ε+2-2-\frac{5\varepsilon^2}{2\varepsilon+2}0
s0s^05

Only the first element of the s3s^3 row is zero (the row is not all zero), so it is replaced by a small positive number ε\varepsilon. Let ε→0+\varepsilon \to 0^+:

RowFirst-column sign
s5s^5+1+1
s4s^4+1+1
s3s^3+ε+\varepsilon
s2s^22ε→+∞\frac{2}{\varepsilon} \to +\infty
s1s^1→−2\to -2
s0s^0+5+5

There are 2 sign changes (+∞→−2+\infty \to -2 and −2→+5-2 \to +5).

Answer: two roots lie in the right half s-plane, so the system is unstable. The other three roots are in the LHP. The actual roots are ≈0.72±j1.17\approx 0.72\pm j1.17, −0.60±j1.34-0.60\pm j1.34 and −1.24-1.24.

  • 2080 Bhadra · 6 marks

The open loop transfer function of a unity feedback system is given by G(s) = k/[s(s+3)(s²+s+1)]. Determine the value of k that will cause sustained oscillation in the closed loop system. Also determine the oscillation frequency.

Answer

Sustained oscillation occurs at the marginal value of kk, where the s1s^1 row of the Routh array is zero. The auxiliary equation from the s2s^2 row then gives the frequency.

Characteristic equation

s(s+3)(s2+s+1)+k=0s4+4s3+4s2+3s+k=0\begin{aligned} s(s+3)(s^2+s+1) + k &= 0 \\ s^4 + 4s^3 + 4s^2 + 3s + k &= 0 \end{aligned}

Routh array

RowCol 1Col 2Col 3
s4s^414kk
s3s^3430
s2s^24(4)−1(3)4=134\frac{4(4)-1(3)}{4}=\frac{13}{4}kk
s1s^1134(3)−4k134=3−16k13\frac{\frac{13}{4}(3)-4k}{\frac{13}{4}}=3-\frac{16k}{13}0
s0s^0kk

For stability: 3−16k13>03-\frac{16k}{13}>0 and k>0k>0, so 0<k<3916=2.43750 < k < \frac{39}{16} = 2.4375.

Value of k for sustained oscillation

3−16k13=0⇒k=3916=2.43753 - \frac{16k}{13} = 0 \Rightarrow k = \frac{39}{16} = 2.4375

Oscillation frequency

Auxiliary equation:

134s2+k=0134s2+3916=0s2=−34⇒s=±j0.866\begin{aligned} \frac{13}{4}s^2 + k &= 0 \\ \frac{13}{4}s^2 + \frac{39}{16} &= 0 \\ s^2 &= -\frac{3}{4} \Rightarrow s = \pm j0.866 \end{aligned}

Check: at k=2.4375k=2.4375 the roots are ±j0.866\pm j0.866, −2.866-2.866 and −1.134-1.134.

Answer: k=2.4375k = 2.4375 gives sustained oscillation at ω=0.866\omega = 0.866 rad/s.

  • 2080 Baisakh · 6 marks

Check for stability of the system using R-H criterion whose characteristic equation is given by q(s) = s⁵ + 2s⁴ + 2s³ + 4s² + s + 2 = 0. Also determine the number of poles in RH plane and on imaginary axis.

Answer

Result: RHP = 0, jωj\omega axis = 4 (±j1\pm j1 repeated), LHP = 1 (s=−2s=-2). The system is unstable.

The Routh array is formed. A row of zeros is handled with the auxiliary polynomial, whose roots are the roots symmetric about the origin.

q(s)=s5+2s4+2s3+4s2+s+2=0q(s) = s^5 + 2s^4 + 2s^3 + 4s^2 + s + 2 = 0

Routh array

RowCol 1Col 2Col 3
s5s^5121
s4s^4242
s3s^32(2)−1(4)2=0\frac{2(2)-1(4)}{2}=02(1)−1(2)2=0\frac{2(1)-1(2)}{2}=0

Zero row. Auxiliary polynomial from the s4s^4 row:

A(s)=2s4+4s2+2,dAds=8s3+8sA(s) = 2s^4 + 4s^2 + 2, \qquad \frac{dA}{ds} = 8s^3 + 8s
RowCol 1Col 2
s3s^388
s2s^28(4)−2(8)8=2\frac{8(4)-2(8)}{8}=28(2)−08=2\frac{8(2)-0}{8}=2
s1s^10 (zero row again)

New auxiliary polynomial A1(s)=2s2+2A_1(s) = 2s^2+2, dA1ds=4s\frac{dA_1}{ds} = 4s:

RowCol 1
s1s^14
s0s^02

First column: 1, 2, 8, 2, 4, 21,\ 2,\ 8,\ 2,\ 4,\ 2. There is no sign change, so no pole is in the RHP.

Poles on the imaginary axis

2s4+4s2+2=2(s2+1)2=0⇒s=±j1, ±j12s^4 + 4s^2 + 2 = 2(s^2+1)^2 = 0 \Rightarrow s = \pm j1,\ \pm j1

The remaining factor is q(s)(s2+1)2=s+2\frac{q(s)}{(s^2+1)^2} = s + 2, giving s=−2s = -2.

RegionNumber of poles
Right half plane0
On jωj\omega axis4 (±j1\pm j1, repeated)
Left half plane1 (s=−2s=-2)

Stability

The poles on the jωj\omega axis are repeated, so the response contains tsin⁡tt\sin t terms that grow with time. The system is unstable, even though no pole is in the RHP.

  • 2078 Bhadra · 2+6 marks

What is relative and absolute stability? Check the stability of system with characteristic equation: s⁶ + 2s⁵ + 8s⁴ + 12s³ + 20s² + 16s + 16 = 0 using R-H criteria.

Answer

Absolute and relative stability

  • Absolute stability answers yes or no: is the system stable or not? A system is absolutely stable if all closed-loop poles lie in the left half of the s-plane, so every bounded input gives a bounded output and the natural response decays to zero. The Routh–Hurwitz criterion checks absolute stability.
  • Relative stability measures how stable a stable system is, i.e. how far its poles are from the jωj\omega axis (instability boundary). Poles further left decay faster and give less oscillation. It is measured by the real part of the dominant poles (settling time), damping ratio, or in the frequency domain by gain margin and phase margin. In Routh's method, it is found by shifting the axis (s=z−σs = z - \sigma) and testing again.
Absolute stabilityRelative stability
Stable or unstable (qualitative)Degree of stability (quantitative)
Checks sign of real parts of polesChecks distance of poles from jωj\omega axis
Routh–Hurwitz, pole locationShifted Routh, GM, PM, damping ratio

Stability of s6+2s5+8s4+12s3+20s2+16s+16=0s^6 + 2s^5 + 8s^4 + 12s^3 + 20s^2 + 16s + 16 = 0

Routh array

RowCol 1Col 2Col 3Col 4
s6s^6182016
s5s^5212160
s4s^42(8)−1(12)2=2\frac{2(8)-1(12)}{2}=22(20)−1(16)2=12\frac{2(20)-1(16)}{2}=1216
s3s^32(12)−2(12)2=0\frac{2(12)-2(12)}{2}=02(16)−2(16)2=0\frac{2(16)-2(16)}{2}=0

The s3s^3 row is all zeros, so there are roots placed symmetrically about the origin. Auxiliary equation from the s4s^4 row:

A(s)=2s4+12s2+16,dAds=8s3+24sA(s) = 2s^4 + 12s^2 + 16, \qquad \frac{dA}{ds} = 8s^3 + 24s
RowCol 1Col 2
s3s^3824
s2s^28(12)−2(24)8=6\frac{8(12)-2(24)}{8}=68(16)−08=16\frac{8(16)-0}{8}=16
s1s^16(24)−8(16)6=2.67\frac{6(24)-8(16)}{6}=2.670
s0s^016

First column: 1, 2, 2, 8, 6, 2.67, 161,\ 2,\ 2,\ 8,\ 6,\ 2.67,\ 16. No sign change, so no root is in the RHP.

Roots of the auxiliary equation

2s4+12s2+16=2(s2+2)(s2+4)=0s=±j1.414, ±j2\begin{aligned} 2s^4+12s^2+16 &= 2(s^2+2)(s^2+4) = 0 \\ s &= \pm j1.414,\ \pm j2 \end{aligned}

These four roots lie on the jωj\omega axis and are not repeated. The other factor is

s6+2s5+8s4+12s3+20s2+16s+16(s2+2)(s2+4)=s2+2s+2  ⇒  s=−1±j1\frac{s^6+2s^5+8s^4+12s^3+20s^2+16s+16}{(s^2+2)(s^2+4)} = s^2+2s+2 \;\Rightarrow\; s = -1\pm j1
RegionNumberRoots
Right half plane0none
jωj\omega axis4±j1.414\pm j1.414, ±j2\pm j2
Left half plane2−1±j1-1\pm j1

Conclusion

There is no root in the RHP, and the four roots on the jωj\omega axis are simple (non-repeated). The system is marginally stable (not absolutely stable): its response contains sustained oscillations at ω=1.414\omega = 1.414 rad/s and ω=2\omega = 2 rad/s.

  • 2076 Chaitra · 5+3 marks

The open loop TF of a unity feedback control system is given as G(s) = k/[s(s²+s+1)(s+2) + k]. Determine the range of gain k for the system to be stable. Also determine the value of k which will cause the sustained oscillation and corresponding oscillation frequency.

Answer

Reading of the question: as printed, ks(s2+s+1)(s+2)+k\frac{k}{s(s^2+s+1)(s+2)+k} is the closed-loop transfer function of a unity feedback system whose open-loop TF is G(s)=ks(s2+s+1)(s+2)G(s) = \frac{k}{s(s^2+s+1)(s+2)}. So the characteristic equation is s(s2+s+1)(s+2)+k=0s(s^2+s+1)(s+2) + k = 0.

Characteristic equation

s(s2+s+1)(s+2)+k=0s(s3+3s2+3s+2)+k=0s4+3s3+3s2+2s+k=0\begin{aligned} s(s^2+s+1)(s+2) + k &= 0 \\ s(s^3 + 3s^2 + 3s + 2) + k &= 0 \\ s^4 + 3s^3 + 3s^2 + 2s + k &= 0 \end{aligned}

Routh array

RowCol 1Col 2Col 3
s4s^413kk
s3s^3320
s2s^23(3)−1(2)3=73\frac{3(3)-1(2)}{3}=\frac{7}{3}kk
s1s^173(2)−3k73=14−9k7\frac{\frac73(2)-3k}{\frac73}=\frac{14-9k}{7}0
s0s^0kk

Range of k for stability

  • s1s^1 row: 14−9k>0⇒k<149=1.55614 - 9k > 0 \Rightarrow k < \frac{14}{9} = 1.556
  • s0s^0 row: k>0k > 0
0<k<1.5560 < k < 1.556

Sustained oscillation

The system oscillates (is marginally stable) when the s1s^1 row is zero:

kmar=149=1.556k_{mar} = \frac{14}{9} = 1.556

Auxiliary equation from the s2s^2 row:

73s2+149=0s2=−149×37=−23ω=2/3=0.816 rad/s\begin{aligned} \frac{7}{3}s^2 + \frac{14}{9} &= 0 \\ s^2 &= -\frac{14}{9}\times\frac{3}{7} = -\frac{2}{3} \\ \omega &= \sqrt{2/3} = 0.816\ \text{rad/s} \end{aligned}

Check: at k=14/9k = 14/9 the roots are ±j0.816\pm j0.816 and −1.5±j0.289-1.5 \pm j0.289.

Answer: stable for 0<k<1.5560<k<1.556; sustained oscillation at k=1.556k = 1.556 with frequency ω=0.816\omega = 0.816 rad/s.

If G(s)G(s) is taken literally as the open-loop TF with unity feedback, the characteristic equation becomes s(s2+s+1)(s+2)+2k=0s(s^2+s+1)(s+2) + 2k = 0. Every kk above is then halved (0<k<0.7780<k<0.778, kmar=0.778k_{mar}=0.778), and the frequency stays the same, 0.816 rad/s.

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.

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