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Tracking, disturbance rejection and pole sensitivity

Short answer

i) Yes, the system is Type 1, giving zero steady-state step error. ii) No, disturbance enters after the controller; steady error = 30/640 ≈ 0.047w. iii) Sensitivity S = -2s(s+30)/(s³+32s²+220s+640), zero at DC.

For a closed loop system given by the block diagram below: i) Can the system track a step reference input 'r' with zero steady state error? ii) Can the system reject a step disturbance 'w' with zero steady state error? iii) Compute the sensitivity of closed loop transfer function to change in the plant pole at '−2'. [Figure: R → summing point (+, −) → controller 160(s+4)/(s+30) → summing point (+, + with disturbance w) → plant 1/[s(s+2)] → y; unity negative feedback from y]

Controller D(s)=160(s+4)s+30D(s) = \dfrac{160(s+4)}{s+30}, plant P(s)=1s(s+2)P(s) = \dfrac{1}{s(s+2)}.

Stability first

Characteristic equation 1+DP=01 + DP = 0:

s(s+2)(s+30)+160(s+4)=s3+32s2+220s+640=0s(s+2)(s+30) + 160(s+4) = s^3 + 32s^2 + 220s + 640 = 0

Routh array:

RowCol 1Col 2
s3s^31220
s2s^232640
s1s^1(32⋅220−640)/32=200(32\cdot 220 - 640)/32 = 2000
s0s^0640

No sign change, so the closed loop is stable and the final value theorem can be used.

i) Tracking a step reference

G(s)=DP=160(s+4)s(s+2)(s+30)G(s) = DP = \frac{160(s+4)}{s(s+2)(s+30)}

There is one pole at the origin, so the system is Type 1: Kp=∞K_p = \infty.

ess=11+Kp=0e_{ss} = \frac{1}{1 + K_p} = 0

Yes, the system tracks a step reference with zero steady state error.

ii) Rejecting a step disturbance ww

With r=0r = 0:

Y(s)W(s)=P1+DP=s+30s3+32s2+220s+640\frac{Y(s)}{W(s)} = \frac{P}{1 + DP} = \frac{s+30}{s^3 + 32s^2 + 220s + 640}

For a unit step W(s)=1/sW(s) = 1/s:

yss=lim⁡s→0s⋅1s⋅s+30s3+32s2+220s+640=30640=0.0469y_{ss} = \lim_{s\to 0} s\cdot\frac{1}{s}\cdot\frac{s+30}{s^3+32s^2+220s+640} = \frac{30}{640} = 0.0469

No. The disturbance enters after the controller, and the integrator is in the plant, not in the controller. So a steady error of 0.0469w0.0469w (about 4.7% of the disturbance) remains.

iii) Sensitivity to the plant pole at −2-2

Let the pole be at −a-a, with a=2a = 2: P=1s(s+a)P = \dfrac{1}{s(s+a)}, T=DP1+DPT = \dfrac{DP}{1+DP}. By the chain rule:

SaT=SPT⋅SaPS_a^T = S_P^T \cdot S_a^P SPT=11+DP=s(s+2)(s+30)s3+32s2+220s+640SaP=∂P∂a⋅aP=−1s(s+a)2⋅a s(s+a)=−as+a=−2s+2\begin{aligned} S_P^T &= \frac{1}{1 + DP} = \frac{s(s+2)(s+30)}{s^3 + 32s^2 + 220s + 640} \\ S_a^P &= \frac{\partial P}{\partial a}\cdot\frac{a}{P} = \frac{-1}{s(s+a)^2}\cdot a\,s(s+a) = \frac{-a}{s+a} = \frac{-2}{s+2} \end{aligned}

Answer:

SaT=−2s(s+30)s3+32s2+220s+640S_a^T = \frac{-2s(s+30)}{s^3 + 32s^2 + 220s + 640}

At DC (s=0s = 0) the sensitivity is zero, so a change in the pole location has no effect on the steady state output. Its effect grows at higher frequencies.

✓ Answer checked by Claude Opus 5.5 (high effort)

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