Control system miscellaneous
- The first two rows of Routh's tabulation of a third order equation are as follows.
s3 2 2 s3 4 4
This means there are
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Two roots at s = ±j and one in left halfs-plane
s3 2 2 s3 4 4
Characteristic equation is A(s) = 2s3 + 4s2 + 2s + 4 = 0
⇒ s3 + 2s2 + s + 2 = 0
⇒ (s + 2) (s2 + 1) = 0
⇒ s = – 2, s = ± j
Correct Option: D
Two roots at s = ±j and one in left halfs-plane
s3 2 2 s3 4 4
Characteristic equation is A(s) = 2s3 + 4s2 + 2s + 4 = 0
⇒ s3 + 2s2 + s + 2 = 0
⇒ (s + 2) (s2 + 1) = 0
⇒ s = – 2, s = ± j
- The asymptotic approximation of the log-magnitude vs frequency plot of a system containing only real poles and zeros is shown in the figure given below. Its transfer function is
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At ω = 0.1, 2 poles At ω = 2, 1 pole At ω = 5 , 1 zero At ω = 25 , 1 pole
So, transfer function,T(s) = k(s + 5) s(s + 2)(s + 25) ∴ 80 = 20 log 5k (0.1)2 × 2 × 25 ⇒ 4 = log 5k 0.5
⇒ 10k = 104
⇒ k = 103 = 1000∴ T(s) = 1000 (s + 5) s2(s + 2)(s + 25)
Correct Option: B
At ω = 0.1, 2 poles At ω = 2, 1 pole At ω = 5 , 1 zero At ω = 25 , 1 pole
So, transfer function,T(s) = k(s + 5) s(s + 2)(s + 25) ∴ 80 = 20 log 5k (0.1)2 × 2 × 25 ⇒ 4 = log 5k 0.5
⇒ 10k = 104
⇒ k = 103 = 1000∴ T(s) = 1000 (s + 5) s2(s + 2)(s + 25)
- The unit -step response of a unity feedback system with open loop transfer function
G(s) = K is shown in the figure below. (s + 1)(s + 2)
The value of K is
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Given : G(s) = K (s + 1)(s + 2)
From curve, steady state error = 1 – 0.75 = 0.25∴ E(s) = R(s) = 1 s 1 + H(s)G(s) 1 + 1. k × 1 (s + 1)(s + 2) ⇒ 1 = 0.25 1 + k 2 ⇒ 1 = 0.25 + 0.25k 2 ⇒ k = 0.75 × 2 = 6 0.25 Correct Option: D
Given : G(s) = K (s + 1)(s + 2)
From curve, steady state error = 1 – 0.75 = 0.25∴ E(s) = R(s) = 1 s 1 + H(s)G(s) 1 + 1. k × 1 (s + 1)(s + 2) ⇒ 1 = 0.25 1 + k 2 ⇒ 1 = 0.25 + 0.25k 2 ⇒ k = 0.75 × 2 = 6 0.25
- The open loop transfer function of a unity feedback system is given by
G(s) = (e-0.1s) s
The gain margin of this system is
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Given : G(s) = e-0.1s s ⇒ G(jω) = e-0.1jω jω
Phase crossover frequency :-90 - 0.1 ω × 180 = - 180 π ⇒ 18 ω = 90 π
⇒ ω = 5π = 15.7 rad/sec
Gain margin :a = |G(jω)|at ω = 18.7 = 1 = 1 ω 15.7
∴ Gain margin = 20 log a= 20 log 1 = -23.9 dB 15.7
Correct Option: D
Given : G(s) = e-0.1s s ⇒ G(jω) = e-0.1jω jω
Phase crossover frequency :-90 - 0.1 ω × 180 = - 180 π ⇒ 18 ω = 90 π
⇒ ω = 5π = 15.7 rad/sec
Gain margin :a = |G(jω)|at ω = 18.7 = 1 = 1 ω 15.7
∴ Gain margin = 20 log a= 20 log 1 = -23.9 dB 15.7
- The characteristic equation of a (3 × 3) matrix P is defined as
α (λ) = |λI – P| = λ3 + λ2 + 2λ + 1 = 0.
If I denotes identity matrix, then the inverse of matrix P will be
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By Clayey – Hamilton theorem,
Every square matrix satisfies its own characteristic equation
α (λ) = λ 3 + λ2 + 2λ + 1 = 0
α(P) = P3 + P2 + 2P + I = 0
⇒ I = – P3 + P2 + 2P
Premultiplying by p-1, we get
P -1 = – [P2 + P + 2I]Correct Option: D
By Clayey – Hamilton theorem,
Every square matrix satisfies its own characteristic equation
α (λ) = λ 3 + λ2 + 2λ + 1 = 0
α(P) = P3 + P2 + 2P + I = 0
⇒ I = – P3 + P2 + 2P
Premultiplying by p-1, we get
P -1 = – [P2 + P + 2I]