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22-Mec-A3 System Analysis and Control · May 2013

Question 4 of 6: Stability range, and the stabilising effect of a feedback zero

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

Notes on this paper

Paper: National Exams — May 2013 · 07-Mec-A3 System Analysis and Controls · 3 hours · closed book (Casio/Sharp calculator + semi-log graph paper only) · any four of six questions constitute a complete paper; all questions of equal value. All six questions are solved here as a study resource.

Reference texts (subject). K. Ogata, Modern Control Engineering, 5th ed. (root locus Ch. 6, frequency response/Bode Ch. 7, steady-state error §5.8, Routh–Hurwitz §5.6); N. S. Nise, Control Systems Engineering, 8th ed.; R. C. Dorf & R. H. Bishop, Modern Control Systems, 13th ed.; G. F. Franklin, J. D. Powell & A. Emami-Naeini, Feedback Control of Dynamic Systems, 7th ed. Laplace-transform pairs are supplied with the exam.

Question 4: Stability range, and the stabilising effect of a feedback zero (equal value)

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. Open-loop transfer function of a unity-feedback system

$$G(s)=\frac{K}{s\,(0.5s+1)\,(2s+1)}.$$

Find. (i) the range of $K$ for stability with unity feedback; (ii) show that replacing the feedback by $H(s)=s+3$ enlarges the stable range.

Approach. Form the characteristic polynomial for each feedback and apply Routh–Hurwitz; compare the resulting upper limits on $K$.

  1. Unity feedback — characteristic polynomial. Since $s(0.5s+1)(2s+1)=s^{3}+2.5s^{2}+s$, $$1+G=0\;\Longrightarrow\;\boxed{\,s^{3}+2.5s^{2}+s+K=0\,}.$$
  2. Unity feedback — Routh test.
    $s^{3}$$1$$1$
    $s^{2}$$2.5$$K$
    $s^{1}$$\dfrac{2.5-K}{2.5}$$0$
    $s^{0}$$K$
    Positivity needs $K>0$ and $2.5-K>0$, so $$\boxed{\,0<K<2.5\,}.$$ The imaginary-axis crossing is at $K=2.5$, $\omega=\sqrt{1/(0.5\cdot2)}=1$ rad/s.
  3. Feedback $H(s)=s+3$ — characteristic polynomial. Now $1+G(s)H(s)=0$ gives $s(0.5s+1)(2s+1)+K(s+3)=0$, i.e. $$\boxed{\,s^{3}+2.5s^{2}+(1+K)s+3K=0\,}.$$ The feedback zero at $s=-3$ raises the $s^{1}$ coefficient from $1$ to $(1+K)$, adding phase lead.
  4. Feedback $H(s)=s+3$ — Routh test.
    $s^{3}$$1$$1+K$
    $s^{2}$$2.5$$3K$
    $s^{1}$$\dfrac{2.5(1+K)-3K}{2.5}=\dfrac{2.5-0.5K}{2.5}$$0$
    $s^{0}$$3K$
    Positivity needs $K>0$ and $2.5-0.5K>0$, so $$\boxed{\,0<K<5\,}.$$
  5. Comparison. The derivative (lead) action of the feedback zero doubles the upper gain limit from $2.5$ to $5$: $$\text{unity: }0<K<2.5\quad\longrightarrow\quad H=s+3:\ 0<K<5.$$ The added zero contributes positive phase, so the loop tolerates twice the gain before its high-frequency poles drive it unstable — the stability range is increased, as required.
FeedbackCharacteristic polynomialStable range
$H=1$$s^{3}+2.5s^{2}+s+K$$0<K<2.5$
$H=s+3$$s^{3}+2.5s^{2}+(1+K)s+3K$$0<K<5$