22-Mec-A3 System Analysis and Control · December 2019
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. National Examination 16-Mec-A3 — System Analysis and Control, December 2019. Three hours; closed book; no aids other than semi-logarithmic graph paper and an approved Casio or Sharp calculator. Six questions are printed and any four constitute a complete paper, all of equal value (25 marks each); only the first four questions appearing in the answer book are marked. A table of Laplace transforms is supplied with the paper. All six questions are solved here, so the set works as a complete study resource rather than one candidate’s four choices.
Reference texts. K. Ogata, Modern Control Engineering, 5th ed. (Pearson) — Chs. 2 (Laplace modelling), 5 (transient response), 6 (root locus), 7 (frequency response); N. S. Nise, Control Systems Engineering, 8th ed. (Wiley) — Chs. 2, 4, 6, 7, 8, 10; G. F. Franklin, J. D. Powell and A. Emami-Naeini, Feedback Control of Dynamic Systems, 8th ed. (Pearson) — Chs. 3, 5, 6; R. C. Dorf and R. H. Bishop, Modern Control Systems, 13th ed. (Pearson). These are the standard references for the 16-Mec-A3 syllabus; the exam is closed book, so every result below is obtained with the supplied Laplace-transform table and hand methods only.
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. Unity negative feedback with forward transfer function $G(s) = \dfrac{10}{s^{2}\left(4+s\right)}$ (Fig 2.0), driven by (a) the ramp $r(t)=10t$ and (b) the combined input $r(t)=4+6t+3t^{2}$.
Find. The steady-state error $e_{ss} = \lim_{t\to\infty}\left[r(t)-c(t)\right]$ for each input.
Approach. Classify the loop by type, evaluate the three static error constants, apply the final-value theorem term by term — and then test the closed-loop characteristic equation with the Routh criterion, because the final-value theorem is only valid for a stable loop.
The two results must be read together. The error constants are perfectly well defined and give the textbook answers $e_{ss}=0$ for the ramp and $e_{ss}=2.4$ for the parabolic input, and those are the values the marking scheme expects. But the final-value theorem may only be applied when $sE(s)$ has all its poles in the left half plane, and here it does not: the physical response diverges, oscillating with a growing envelope at about 1.47 rad/s. The complete answer therefore states both the formal error figures and the fact that this particular loop can never reach them.
Check: the printed loop is unstable as drawn. In an examination answer, quote the error constants, then note explicitly that the steady-state error is only realisable if the loop is first stabilised — for instance by cascading a phase-lead network such as $D(s)=(1+\alpha s)$, which supplies the missing $s$ coefficient. Adding a single zero at $s=-1$ makes the characteristic polynomial $s^{3}+4s^{2}+10s+10$, whose Routh first column is all positive.
| Quantity | Value | Remark |
|---|---|---|
| System type | 2 | double pole at the origin |
| $K_p$ | $\infty$ | zero step error |
| $K_v$ | $\infty$ | zero ramp error |
| $K_a$ | $2.5\ \text{s}^{-2}$ | finite parabolic error |
| (a) $e_{ss}$ for $r=10t$ | $0$ | formal value |
| (b) $e_{ss}$ for $r=4+6t+3t^{2}$ | $2.4$ | from the $3t^{2}$ term only |
| Closed-loop stability | unstable (2 RHP poles) | $s^{3}+4s^{2}+10$; errors not physically realised |