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For the system of Figure 2, (a) (2.5 points) Find the system type (b) (4 points) Find the steady-state error for an inpu

Posted: Fri Jul 08, 2022 6:21 am
by answerhappygod
For The System Of Figure 2 A 2 5 Points Find The System Type B 4 Points Find The Steady State Error For An Inpu 1
For The System Of Figure 2 A 2 5 Points Find The System Type B 4 Points Find The Steady State Error For An Inpu 1 (43.67 KiB) Viewed 29 times
For The System Of Figure 2 A 2 5 Points Find The System Type B 4 Points Find The Steady State Error For An Inpu 2
For The System Of Figure 2 A 2 5 Points Find The System Type B 4 Points Find The Steady State Error For An Inpu 2 (47.59 KiB) Viewed 29 times
For the system of Figure 2, (a) (2.5 points) Find the system type (b) (4 points) Find the steady-state error for an input 50u(t), 50tu(t), and 50t²u(t) (c) (3.5 points) Is the system stable? R(s) + 5 s(s+ 1)(s+2) (s + 3) C(s)
Information sheet The Routh table for a polynomial of the form as + a₂s³ + a₂s² + a₂ + a $³ 80 b₁ = 1 1+ Kp 1 K₂ C₁₂ e(∞o) ramp e (co) parabola d₁ = = 1 Ka a4 0+5 a3 Position constant, K₂ = limG (s) 194 laz 5+0 Velocity constant, K, =lim sG(s) az 193 a₂ lb₁ b₂ b₂ 9₂₁₂ Acceleration constant, K₁ = lim s²G(s) System error e(00) step a₂ 0-5 b₂ = d₂ = The final value theorem for a negative unity feedback system e (co) = lim sE (s) = lim sR(s) [1+G(S)] = ! lim Static error constants a₂ 194 laz |a3 |b₁ az b₂ dol 0 -18 C₂ =0 = 0 SR(s) $+01+G(S) b₂ = C3 = d₂ = do 0 a₁ 0 az 0 az az |b₁ 0 b₂ -1 ol C₁ 0 = 0 = 0