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23-Chem-A6 Process Dynamics and Control · December 2019

Question 6 of 8: Routh Stability of a Quartic Characteristic Equation

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Reference texts: D. E. Seborg, T. F. Edgar, D. A. Mellichamp & F. J. Doyle III, Process Dynamics and Control (4th ed., Wiley) — Laplace-domain modelling, linearisation, transfer functions, feedback stability, frequency response and IMC design; G. Stephanopoulos, Chemical Process Control (Prentice Hall) — Routh test, Nyquist criterion and dead-time systems; D. R. Coughanowr & S. E. LeBlanc, Process Systems Analysis and Control (3rd ed., McGraw-Hill) — first-order thermal/level dynamics, step/ramp/pulse response and block-diagram algebra. Standard control conventions (deviation variables; unity valve/sensor gains unless stated) are used throughout. This sitting is an open-book paper of eight problems of which any five constitute a complete exam; all eight are solved here.

Problem 6: Routh Stability of a Quartic Characteristic Equation (20%)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. A fourth-order characteristic polynomial with the gain in the constant term:

Power$s^4$$s^3$$s^2$$s^1$$s^0$
Coefficient$1$$4$$6$$4$$1+K_c$

Find. (a) the stabilising range of $K_c$; (b) the marginal gain(s) and the frequency of sustained oscillation.

Approach. All coefficients are positive only if $1+K_c>0$; the decisive test is the Routh array—require every first-column entry positive, and locate the stability limit where an entry vanishes (an auxiliary polynomial then gives the imaginary-axis crossing).

  1. Build the Routh array. Lay out the first two rows from the coefficients and reduce: $$\begin{array}{c|ccc} s^4 & 1 & 6 & 1+K_c\\ s^3 & 4 & 4 & 0\\ s^2 & b_1 & 1+K_c & \\ s^1 & c_1 & & \\ s^0 & 1+K_c & & \end{array}$$ with $b_1=\dfrac{4\cdot6-1\cdot4}{4}=5$.
  2. Compute the $s^1$ entry. $$c_1=\frac{b_1\cdot4-4\,(1+K_c)}{b_1}=\frac{5\cdot4-4(1+K_c)}{5}=\frac{16-4K_c}{5}.$$ The first column is therefore $\{1,\,4,\,5,\,\tfrac{16-4K_c}{5},\,1+K_c\}$.
  3. (a) Stability conditions. Every first-column entry must be positive. The two binding inequalities are $$\frac{16-4K_c}{5}>0\ \Rightarrow\ K_c<4,\qquad 1+K_c>0\ \Rightarrow\ K_c>-1.$$ Hence $$\boxed{-1<K_c<4.}$$
  4. (b) Upper limit $K_c=4$. At $K_c=4$ the $s^1$ entry vanishes, signalling a pair of poles on the imaginary axis. Form the auxiliary polynomial from the $s^2$ row: $5s^2+(1+K_c)=5s^2+5=0\Rightarrow s^2=-1\Rightarrow s=\pm j$. The loop sustains an undamped oscillation at $$\boxed{K_c=4,\qquad \omega_u=1\ \text{rad/min}.}$$
  5. (b) Lower limit $K_c=-1$. At $K_c=-1$ the constant term $1+K_c=0$, so $s=0$ is a root—a pole migrates through the origin (monotonic, not oscillatory, instability). Physically only positive gains are used, so the operative marginal gain is $K_c=4$.
P6: stability band of the gain $K_c$ $K_c=-1$ $K_c=4$ STABLE : $-1<K_c<4$ unstable unstable pole at origin $\omega_u=1$ rad/min
Problem 6: the Routh test bounds the gain to $-1<K_c<4$. The upper edge $K_c=4$ is an oscillatory (imaginary-axis) limit at $\omega_u=1$ rad/min; the lower edge $K_c=-1$ is a root crossing through the origin.
QuantityValue
(a) Stable range$-1<K_c<4$
(b) Marginal (oscillatory) gain$K_c=4$
(b) Ultimate frequency$\omega_u=1$ rad/min
(b) Lower marginal gain$K_c=-1$ (root at origin)