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20-Bio-A2 Process Dynamics and Control · May 2018

Question 5 of 8: Linearization of a Radiative Calrod Heating Element

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

Notes on this paper

National Exams / EGBC — May 2018 — 04-Bio-A2 Process Dynamics and Control. Three-hour open-book examination; any non-communicating calculator is permitted. The cover page states that only the first five questions in the answer book are marked, yet all eight problems are printed on the paper — all eight are solved below for completeness, since the full set is a study resource. Content spans second-order Bode/phase-margin analysis, feedback stability with a non-minimum-phase sensor, dead-time Nyquist/gain-margin design, zero-location effects on step response, nonlinear radiative-heat-transfer linearization, Internal Model Control (IMC) of a dead-time process, PI-controller stability/response, and nonlinear-CSTR linearization. Note: Problem 2's printed sub-part weights (10%+20%=30%) exceed its stated 20% problem total — both sub-parts are fully answered below.

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, transfer functions, Routh stability, Nyquist/Bode frequency response, linearization and IMC design; G. Stephanopoulos, Chemical Process Control: An Introduction to Theory and Practice (Prentice Hall) — Nyquist criterion and dead-time systems. Standard control conventions (deviation variables; unity valve gain unless stated) are used throughout.

Problem 5: Linearization of a Radiative Calrod Heating Element (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. $mC\,dT/dt=Q-k(T^4-T_a^4)$; steady state $(T_s,T_{as},Q_s)$ with $Q_s=k(T_s^4-T_{as}^4)$; $m$, $C$, $k$ all positive physical constants.

Find. (a) $\delta T(s)/\delta Q(s)$ and $\delta T(s)/\delta T_a(s)$ in standard gain/time-constant form; (b) the required sign of the proportional controller gain $K_c$.

Approach. Perturb about the steady state, linearize the $T^4$ and $T_a^4$ terms by a first-order Taylor expansion ($T^4\approx T_s^4+4T_s^3\delta T$), Laplace-transform the resulting linear ODE, and solve for each transfer function in turn (holding the other input at its steady value). For (b), examine the sign of the process gain and its effect on the closed-loop pole.

  1. Linearize. $T^4\approx T_s^4+4T_s^3\,\delta T$ and $T_a^4\approx T_{as}^4+4T_{as}^3\,\delta T_a$. Substituting and subtracting the steady-state balance leaves $$mC\frac{d(\delta T)}{dt}+4kT_s^3\,\delta T=\delta Q+4kT_{as}^3\,\delta T_a.$$
  2. Laplace transform. $(mCs+4kT_s^3)\,\delta T(s)=\delta Q(s)+4kT_{as}^3\,\delta T_a(s)$.
  3. (a) $\delta T/\delta Q$ (with $\delta T_a=0$). $$\boxed{\frac{\delta T(s)}{\delta Q(s)}=\frac{1}{mCs+4kT_s^3}=\frac{K_1}{\tau s+1},\qquad K_1=\frac{1}{4kT_s^3},\quad \tau=\frac{mC}{4kT_s^3}.}$$
  4. (a) $\delta T/\delta T_a$ (with $\delta Q=0$). $$\boxed{\frac{\delta T(s)}{\delta T_a(s)}=\frac{4kT_{as}^3}{mCs+4kT_s^3}=\frac{K_2}{\tau s+1},\qquad K_2=\left(\frac{T_{as}}{T_s}\right)^3,}$$ using the same time constant $\tau$ as above (both inputs enter the same first-order lag).
  5. (b) Sign of $K_c$. The process gain $K_1=1/(4kT_s^3)$ is strictly positive (all physical quantities are positive): more heat input $Q$ always raises $T$. With proportional feedback, the closed-loop characteristic equation is $\tau s+1+K_cK_1=0\Rightarrow s=-(1+K_cK_1)/\tau$. If $T$ falls below setpoint (positive error), the controller must increase $Q$ to correct it — requiring $K_c\gt0$ for the correct (negative-feedback) control action; a negative $K_c$ would decrease $Q$ on a low-temperature error, driving $T$ further away and, for sufficiently negative $K_c$, pushing $1+K_cK_1<0$ and the pole into the right half-plane. $$\boxed{K_c\gt0\ \text{is required (direct-acting process, correct-sign reverse control action).}}$$
ResultValue
Time constant$\tau=mC/(4kT_s^3)$
Gain $\delta T/\delta Q$$K_1=1/(4kT_s^3)$
Gain $\delta T/\delta T_a$$K_2=(T_{as}/T_s)^3$
Controller sign$K_c\gt0$