C(S)/R(S) = G(S) / 1 + G(S)H(S) H(S) = 1 C(S)/R(S) = K/S(1 + ST) / 1 + K/S(1 + ST) C(S)/R(S) = K/S(1 + ST) + K C(S)/R(S) = K/T / S2 + S/T + K/T For second order system, S2 + 2ξWnS + Wn2 2ξWn = 1/T ξ = 1/2WnT Wn2 = K/T Wn =√K/T ξ = 1 / 2√K/T T ξ = 1 / 2 √KT forξ1 = 0.2, for ξ2 = 0.4 ξ1 = 1 / 2 √K1T ξ2 = 1 / 2 √K2T ξ1/ ξ2 = √K2/K1 K2/K1 = (0.2/0.4)2 K2/K1 = 1 / 4 K1 = 4K2 |
T(s) = = 1 Kv = SG(s) = S = 0
Ka = s2 G(s) = s2 = 0
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ess= = = = 5/3 |
T(s) =
For second order system, S2 + 2ξWnS + Wn2 wn = = 5.1 2ξWn = 5 i) Damping Ratio = 0.49 ii) Maximum overshoot Mp = e-∏ξ / √1 –ξ2 x 100 = e-∏x0.49 / √1 – (0.49)2 = 17.1% iii) Rise Time tr = ∏ - φ/Wd Wd = Wn√1 - ξ2 = 5.1 √1 – (0.49)2 = 4.45 sec φ= tan-1√1 – ξ2 / ξ = 1.059 rad tr = ∏ - φ/Wd = ∏ - 1.059/4.45 =468.53msec
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Mp = e-∏ξ / √1 –ξ2 |
Condition 3 ξ = 1 C (S) = R (S) Wn2 / S2 + 2ξWnS + Wn2 C (S) = Wn2 / S (S2 + 2WnS + Wn2) [ R(S) = 1/S ] C (S) = Wn2 / S (S2 + Wn2) C (t) = 1 – e-Wnt + tWne-Wnt The response is critically damped. (4). Settling Time (ts): ts = 3 / ξWn (5%) ts = 4 / ξWn (2%) Q9) Determine the type and order of the system G(s)= K/S(S+1) G(S)= K(S+1)/S2(S+2) Sol: G(s)= K/S(S+1) It is order 2 and type 1 system G(S)= K(S+1)/S2(S+2) It is order 3 and type 2 system Q10) Derive position error coefficient? Sol: R(s)= Unit step R(t) = u(t) R(s) = 1/s ess = s[ R(s)/1+G(s)] = s[ys/1+G(s)] ess= 1+1/1+G(s) =1/1+lt G(s) s- 0 (Position error coefficient)
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