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 axis at , 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.
All coefficients are present and positive, so the necessary condition is satisfied.
Routh array
| Row | Col 1 | Col 2 | Col 3 | Col 4 |
|---|---|---|---|---|
| 1 | 4 | 5 | 2 | |
| 3 | 6 | 3 | 0 | |
| 2 | ||||
| 0 | 0 |
The row is all zeros. Auxiliary equation from the row:
Replace the row by and continue:
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 8 | 8 | ||
| 0 |
The row is zero again. New auxiliary equation , :
| Row | Col 1 |
|---|---|
| 4 | |
| 2 |
First column: . No sign change, so no root is in the right half plane.
Roots of the auxiliary equation
So is a repeated pair on the imaginary axis. Dividing by leaves .
Location of roots
| Region | Number | Roots |
|---|---|---|
| Right half plane | 0 | none |
| On axis | 4 | (each twice) |
| Left half plane | 2 |
Comment on stability
There is no RHP root, but the imaginary-axis roots are repeated. Repeated poles on the axis give terms like in the response, which grow without limit. Therefore the system is unstable. If the 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 ), axis = 4 (, 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.
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 2 | 1 | |
| 4 | 8 | 4 | |
The row is all zeros. Auxiliary polynomial from the row:
| Row | Col 1 | Col 2 |
|---|---|---|
| 16 | 16 | |
| 0 (zero row again) |
New auxiliary polynomial , :
| Row | Col 1 |
|---|---|
| 8 | |
| 4 |
First column: . No sign change, so there is no root in the RHP.
Roots from the auxiliary polynomial
These 4 roots lie on the axis (repeated pair). The remaining root: , so .
| Region | Number of roots |
|---|---|
| Right half s-plane | 0 |
| Left half s-plane | 1 () |
| On axis | 4 ( repeated) |
Stability
No root is in the RHP, but the roots on the axis are repeated. They produce a response term like , 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 axis. To find out whether all roots lie to the left of a line , the axis is shifted.
Method (axis shifting)
- Take the characteristic equation .
- Substitute , where is the required margin. This moves the vertical line to the new imaginary axis ().
- Expand to get a polynomial .
- Form the Routh array of .
- Number of sign changes = number of roots to the right of .
- No sign change: all roots lie to the left of , so every root has real part more negative than . Each mode then decays at least as fast as .
- A zero row: roots lie exactly on the line .
- Repeat for other values, or keep (or a gain ) as a variable to find the limit.
jw | jw' (new axis)
| |
x | |
x | | Shift: s = z - sigma
------------+---+-------- sigma
x -sigma 0
| |
Example
(roots ). Check whether all roots lie left of . Put :
| Row | Col 1 | Col 2 |
|---|---|---|
| 1 | 5.75 | |
| 4.5 | 1.875 | |
| 5.333 | ||
| 1.875 |
No sign change, so all roots lie to the left of . With , ; the constant term becomes zero, showing a root exactly at .
Uses
- Ensures a minimum decay rate, i.e. settling time .
- Lets the designer find the range of gain 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 in it. For stability, every element of the first column must be positive. Marginal stability occurs when the row becomes zero.
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 15 | ||
| 20 | 2 | 0 | |
| 0 | |||
(i) Range of K for stability
- From row:
- From row:
(ii) Marginal stability
Yes. At the row becomes all zero, and the system has a pair of roots on the axis (marginally stable, sustained oscillation).
Auxiliary equation from the row:
So the frequency of sustained oscillation is rad/s.
Answer: stable for ; marginally stable at , oscillating at 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 and . For this means any when , and when . It just oscillates at , with rad/s.
The characteristic equation is . The Routh array gives the stability conditions in terms of and . Sustained oscillation occurs when the row becomes zero.
Characteristic equation
Routh array
| Row | Col 1 | Col 2 |
|---|---|---|
| 1 | ||
| 0 | ||
Conditions for stability
Interpreting condition 3 (for , ):
- If : condition 3 holds for every , so the system is stable for all .
- If : . A positive range exists only if .
Sustained oscillation
The system just oscillates when the row is zero:
Auxiliary equation from the row:
Example: for : and rad/s. Check: , which has roots .
- 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 is tested with the Routh array. The system just oscillates (is marginally stable) when the row becomes zero.
Characteristic equation
Routh array
| Row | Col 1 | Col 2 |
|---|---|---|
| 1 | ||
| 10 | ||
| 0 | ||
Range of K
- row:
- row:
Sustained oscillation
At the row is zero, so the system just oscillates. Auxiliary equation from the row:
Answer: stable for ; it just oscillates at , with frequency 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 . All first-column Routh elements must be positive.
Characteristic equation
Routh array
| Row | Col 1 | Col 2 |
|---|---|---|
| 1 | ||
| 10 | ||
| 0 | ||
Conditions
- row:
- row:
- From these, (also needed so that all coefficients are positive).
Interpretation: for a given , the gain can be raised up to . At the system is marginally stable and oscillates at rad/s (from ). For example, with the system is stable for .
Answer: relation for stability: (with ).
- 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 , shift the imaginary axis to by putting . Then apply the Routh criterion to the new polynomial in (relative stability).
Characteristic equation
Shift the axis:
Routh array in z
| Row | Col 1 | Col 2 |
|---|---|---|
| 0 | ||
For no sign change (all roots left of , i.e. left of ):
Physical meaning: the sum of the closed-loop roots is , so both roots can be left of only if . The gain must be large enough that the slower real root moves past .
Example: for and : . With , gives , both left of .
- 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 and , one root at , and none in the RHP.
For unity negative feedback, the characteristic equation is . Its Routh array is formed and the first column is examined.
Characteristic equation
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 6 | 8 | |
| 7 | 42 | 56 | |
The row is all zeros. Auxiliary equation from the row:
| Row | Col 1 | Col 2 |
|---|---|---|
| 28 | 84 | |
| 56 | ||
| 56 |
First column: . No sign change, so no root is in the RHP.
Roots on the imaginary axis
The fifth root: , so .
| Region | Roots |
|---|---|
| RHP | none |
| axis | , (non-repeated) |
| LHP |
Conclusion
The poles on the 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, axis = 0. The system is unstable.
For unity negative feedback the characteristic equation is . 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
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 11 | 200 | |
| 6 | 6 | 0 | |
| 0 | |||
| 200 |
First column: .
Sign changes: (one) and (two), so there are 2 sign changes.
Root location
| Region | Number of roots |
|---|---|
| Right half s-plane | 2 |
| Left half s-plane | |
| On axis | 0 (no zero row) |
The numerical roots ( and ) 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 row then becomes zero, and the auxiliary equation from the row gives the frequency of oscillation.
Characteristic equation
Routh array
| Row | Col 1 | Col 2 |
|---|---|---|
| 1 | ||
| 0 | ||
Condition for sustained oscillation
row :
Auxiliary equation from the row, with :
From (1), , so (2) becomes .
Substitute rad/s
Check
With , : . The roots are and , so the system oscillates at 2 rad/s.
Answer: , .
- 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 adds a term to the response.
| Pole location | Response term | Stability |
|---|---|---|
| Left half plane () | Decays to zero | Stable |
| Simple poles on axis | Constant or steady oscillation | Marginally stable |
| Repeated poles on axis | , grows | Unstable |
| Right half plane () | Grows exponentially | Unstable |
- The further left the poles are, the faster the response decays. This means greater relative stability.
- Poles close to the axis (dominant poles) decay slowly and decide the transient response.
- Imaginary part 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 .
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 2 | 2 | 2 | |
| 3 | 1 | 2 | |
| 0 | |||
| 0 | |||
| 2 |
First column: .
There are 2 sign changes ( and ), 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 , and .
- 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 and make every first-column element positive.
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 25 | ||
| 2 | 9 | 0 | |
| 25 | |||
| 0 | |||
| 25 |
Conditions
- row:
- row: with , we need
- row: always true.
Condition 2 is stricter, so:
Marginal value
At , the row is zero. The auxiliary equation gives , so the system would oscillate at 2.12 rad/s.
Answer: the system is stable for (i.e. ). 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 adds a pole at the origin. Find the closed-loop characteristic equation and apply Routh's criterion.
Characteristic equation
Routh array
| Row | Col 1 | Col 2 |
|---|---|---|
| 1 | ||
| 3 | ||
| 0 | ||
Conditions for stability
- row:
- row:
- This also requires .
Example: with , the integral gain must satisfy ; with , . A larger allows a larger .
- 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 , with .
Characteristic equation
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 3 | ||
| 3 | 2 | 0 | |
| 0 | |||
Conditions
- row:
- row:
At the system is marginally stable. The auxiliary equation gives rad/s.
Answer: stable for (= 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): , . In general, and .
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
Routh array
| Row | Col 1 | Col 2 |
|---|---|---|
| 1 | ||
| 0 | ||
Conditions for sustained oscillation
The row must be zero:
Auxiliary equation (from the row) with :
From (1) and (2): .
Substitute rad/s
Check: . The roots are and , so the system oscillates at 2 rad/s.
Answer: , . In general: and . The system is stable when .
- 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, 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.
Routh array
| Row | Col 1 | Col 2 | Col 3 | Col 4 |
|---|---|---|---|---|
| 1 | 8 | 20 | 16 | |
| 2 | 12 | 16 | 0 | |
| 16 | ||||
The row is all zeros, so there are roots placed symmetrically about the origin. Auxiliary equation from the row:
| Row | Col 1 | Col 2 |
|---|---|---|
| 8 | 24 | |
| 0 | ||
| 16 |
First column: . No sign change, so no root is in the RHP.
Roots of the auxiliary equation
These four roots lie on the axis and are not repeated. The other factor is
| Region | Number | Roots |
|---|---|---|
| Right half plane | 0 | none |
| axis | 4 | , |
| Left half plane | 2 |
The -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.
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
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 18 | 50 | |
| 8 | 16 | 0 | |
| 0 | |||
| 50 |
Examination of the first column
First column:
- : first sign change
- : second sign change
2 sign changes, so 2 roots lie in the right half of the s-plane.
| Region | Number of roots |
|---|---|
| Right half plane | 2 |
| Left half plane | 2 |
| axis | 0 |
The actual roots are and , 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 when . There is no finite maximum; is the limiting value.
To check that all poles lie to the left of , shift the imaginary axis to by putting . Then apply the Routh criterion in . Unity feedback is assumed.
Characteristic equation
Shift:
Routh array in z
| Row | Col 1 | Col 2 |
|---|---|---|
| 1 | ||
| 3.5 | ||
| 0 | ||
Conditions
- row: (true for )
- row:
So all closed-loop poles lie to the left of when
Comment on "maximum K"
For this system there is no finite maximum. As , one pole moves to the zero at , and the other two follow asymptotes at from the centroid , which is left of . The limiting (boundary) value is . At the poles are and , so one pole is exactly at .
Answer: all poles lie left of for ; the boundary value is .
- 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 . The system is stable when the first column of the Routh array has no sign change.
Characteristic equation
Routh array
| Row | Col 1 | Col 2 |
|---|---|---|
| 1 | ||
| 10 | ||
| 0 | ||
Conditions for stability
- From the row:
- From the row:
Marginal stability
At the row vanishes. Auxiliary equation:
So at the system oscillates at 9.54 rad/s, and for two poles move into the RHP.
Answer: the system is stable for .
- 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 and apply the Routh criterion. Sustained oscillation occurs when the row becomes zero, and the auxiliary equation from the row gives the frequency.
Characteristic equation
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 69 | ||
| 12 | 198 | 0 | |
| 0 | |||
Range of K
- row:
- row:
Value of K for sustained oscillation
Frequency of oscillation
Auxiliary equation from the row:
Check: with the roots are and .
Answer: stable for ; sustained oscillation at with 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, 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 axis.
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 5 | 1 | |
| 3 | 4 | 3 | |
| 0 | |||
| 3 |
First column: .
- : one sign change
- : second sign change
Root distribution
No row became entirely zero, so no root lies on the axis.
| Region | Number of roots |
|---|---|
| Right half plane | 2 |
| axis | 0 |
| Left half plane |
The roots (, , ) confirm this.
Answer: 2 roots in the RHP, 3 in the LHP, none on the 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 " means all closed-loop poles must lie to the left of the line . Shift the imaginary axis by putting , then apply the Routh criterion in .
Characteristic equation
Shift the axis:
Routh array in z
| Row | Col 1 | Col 2 |
|---|---|---|
| 1 | ||
| 0 | ||
Conditions
- row:
- row:
Both must hold, so
Check: at , gives , exactly on the line . For the real part of the roots (or both real roots) is more negative than .
Answer: all roots are more negative than for .
- 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 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 () and testing again.
| Absolute stability | Relative stability |
|---|---|
| Stable or unstable (qualitative) | Degree of stability (quantitative) |
| Checks sign of real parts of poles | Checks distance of poles from axis |
| Routh–Hurwitz, pole location | Shifted Routh, GM, PM, damping ratio |
Stability of
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 2 | 3 | |
| 1 | 2 | 5 | |
| 5 | |||
| 0 | |||
| 5 |
Only the first element of the row is zero (the row is not all zero), so it is replaced by a small positive number . Let :
| Row | First-column sign |
|---|---|
There are 2 sign changes ( and ).
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 , and .
- 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 , where the row of the Routh array is zero. The auxiliary equation from the row then gives the frequency.
Characteristic equation
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 4 | ||
| 4 | 3 | 0 | |
| 0 | |||
For stability: and , so .
Value of k for sustained oscillation
Oscillation frequency
Auxiliary equation:
Check: at the roots are , and .
Answer: gives sustained oscillation at 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, axis = 4 ( repeated), LHP = 1 (). 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.
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 2 | 1 | |
| 2 | 4 | 2 | |
Zero row. Auxiliary polynomial from the row:
| Row | Col 1 | Col 2 |
|---|---|---|
| 8 | 8 | |
| 0 (zero row again) |
New auxiliary polynomial , :
| Row | Col 1 |
|---|---|
| 4 | |
| 2 |
First column: . There is no sign change, so no pole is in the RHP.
Poles on the imaginary axis
The remaining factor is , giving .
| Region | Number of poles |
|---|---|
| Right half plane | 0 |
| On axis | 4 (, repeated) |
| Left half plane | 1 () |
Stability
The poles on the axis are repeated, so the response contains 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 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 () and testing again.
| Absolute stability | Relative stability |
|---|---|
| Stable or unstable (qualitative) | Degree of stability (quantitative) |
| Checks sign of real parts of poles | Checks distance of poles from axis |
| Routh–Hurwitz, pole location | Shifted Routh, GM, PM, damping ratio |
Stability of
Routh array
| Row | Col 1 | Col 2 | Col 3 | Col 4 |
|---|---|---|---|---|
| 1 | 8 | 20 | 16 | |
| 2 | 12 | 16 | 0 | |
| 16 | ||||
The row is all zeros, so there are roots placed symmetrically about the origin. Auxiliary equation from the row:
| Row | Col 1 | Col 2 |
|---|---|---|
| 8 | 24 | |
| 0 | ||
| 16 |
First column: . No sign change, so no root is in the RHP.
Roots of the auxiliary equation
These four roots lie on the axis and are not repeated. The other factor is
| Region | Number | Roots |
|---|---|---|
| Right half plane | 0 | none |
| axis | 4 | , |
| Left half plane | 2 |
Conclusion
There is no root in the RHP, and the four roots on the axis are simple (non-repeated). The system is marginally stable (not absolutely stable): its response contains sustained oscillations at rad/s and 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, is the closed-loop transfer function of a unity feedback system whose open-loop TF is . So the characteristic equation is .
Characteristic equation
Routh array
| Row | Col 1 | Col 2 | Col 3 |
|---|---|---|---|
| 1 | 3 | ||
| 3 | 2 | 0 | |
| 0 | |||
Range of k for stability
- row:
- row:
Sustained oscillation
The system oscillates (is marginally stable) when the row is zero:
Auxiliary equation from the row:
Check: at the roots are and .
Answer: stable for ; sustained oscillation at with frequency rad/s.
If is taken literally as the open-loop TF with unity feedback, the characteristic equation becomes . Every above is then halved (, ), 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.
Chapter titles and hours from the IOE syllabus ↗