Please consider the following closed-loop Multiple-Input Multiple-Output (MIMO) control system:R₁(s) and R2(s) are the reference signals (or inputs),•G₁(s) (where i = 1,2,3,4,5) are the plant transfer functions,•C₁(s) and C2(s) are the responses (or system outputs),•All of them are in Laplace domain.R2+R₁ ++G₂(s)G3(S)Tasks:G5(s)G4(s)+G₁(s)میa) Please derive the transfer function between C₁ (s) and R₂(s) (i.e., findR₂(s)(10 marks)(10 marks)b) Please derive the transfer function between C₂(s) and R₁(s) (i.e., find C2 (s)).R₁(s)Hint: Please carefully analyse how the signals interact with the plants G₁(s) and find all paths from

Answered: Please consider the following…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Please solve this question in mechatronics
(1) Consider the system represented by the block diagram. The closed loop transfer function T(s)-Y(s)/R(s) is (a) T(s)-50/(s+55 s+50). (b) T(s)=10/(s+50 s+55) (c) T(s)=10/(s+55 s+10). (d) None of the above. R(s)- 10 + s+5 5 Y(s)
The arm angle, e (t), is controlled by a closed-loop system. The input (reference) to the system is the desired angle, and the output is the actual angle. A controller uses the difference between the desired angle and the actual angle to drive the motor, resulting in a motor torque applied to the system. motor torque(tm) shoulder joint damping(B) Arm length (1) g The customer wants to make a system to have 1) O steady-state error 2) Less than 10% overshoot 3) Less than 1 secs of settling time For a step input. Mass(m)
The arm angle, e (t), is controlled by a closed-loop system. The input (reference) to the system is the desired angle, and the output is the actual angle. A controller uses the difference between the desired angle and the actual angle to drive the motor, resulting in a motor torque applied to the system. motor torque(t) houlder joint damping(B) The customer wants to make a system to have 1) O steady-state error 2) Less than 10% overshoot 3) Less than 1- For a step inp **ling time Arm length (/) Mass(m) g design a controller to meet the design spec above. 1) Design a controller to meet the design spec. 2) Evaluate your controller using step response (time response) 3) Evaluate your closed-loop system using frequency response (e.g., Bandwidth, Gain margin. Phase margin).
QUESTION 5 Consider the system whose block diagram is shown below. D(s) R(s) + + C(s) K G(s) G(8) R(s) is the reference input or target, and D(s) is the disturbance input. Gp(t) is the plant (house, motor, car,...) transfer function, Gc(t) is the compensator transfer function, and K is the compensator gain given by 1 G (s) G (s) = P s+10 1 3s+2 and K=5. Find the transfer function, C(s)/R(s). 3 s²+16s+14 8 3s²+32s+25 S 382+8+6 8(s+ 10) 3s² + 32s+25 3s+2 3s²+32s+25 5 3x²+32x+25
6. The figure below represents a time response of a control system. y(r) 0.63 What is it? a) Unit-step response of a Prototype First-Order System; b) Unit-Impulse Response of a Prototype First-Order System; c) Unit-Step Response of a Prototype Second-Order System; d) Unit-Impulse Response of a Prototype Second-Order System.
QUESTION 1 Given a system model, d²x (t) dx (1) dt² dt x (0) = 1 dx (1) dt +2- +x(t) =f(t) t=0 What is the transfer function, X(s)/F(s)? O X(s) s² + s+1 F(s) 1 O X (s) F(s) O X (s) F(s) = 0. X (s) F(s) = 1 s²+2s+1 1 s²+1 S s²+2s+1
A) Find and plot closed-loop pole locations of the system below for K=0, 10, 25, 40, 50 B) Calculate the angles and magnitude of the open-loop transfer function for each of the poles depending on the K above. C) Plot closed loop time response for each closed loop transfer function for K = 0, 10, 25, 40, 50. D) Discuss the transient response: pole locations and time response. E) Discuss the steady-state response. R(s) + Ꮎ C Р • Controller C = K Plant P = 16 s(s + 10) Octave is allowed
Problem 3. Consider the electrical circuit shown in Figure 3 (left). Assume that R₁ = R2 = 1 and C = 1F. 1) (15 points) Derive the transfer function G(s) = Vo(s)/Vs(s) of the electrical circuit. 2) (15 points) If a controller is used to control the system, then the block diagram of the closed-loop system is given by Fig. 3 (right). Suppose that the reference is a ramp signal, i.e., r(t) = t 1(t). Design a controller De(s) such that the closed-loop system achieves perfect tracking (e(t) = r(t) - y(t) → 0). Justify your design. a -> + US R₁i w C: iz iz i3 + R2 Vo RO Σ Do(s) G(s) OY Figure 3: Electrical system in Problem 3.
Below is a very common feedback block system. It is a 1dof, and unity-feedback system. The input is the reference command R(s). This is what flows out of thin air, into the system. All other signals in the system (e.g. U, Y, etc.) will depend on R(s). R(s) a. E(s) e. K U(s) G Y(s) Write the algebraic relation between the output Y(s) and the reference R(s) in terms of G and K?. Write it in the format Y = some function of s * R b. What is the TF from R to Y, aka the closed loop TF? What is the "Loop TF" aka the "the open-loop TF"? G has zeros at ZG1, ZG2 etc. and poles at PG1, PG2 etc. C. K has zeros at ZK1, ZK2 etc. and poles at PK1, PK2 etc. What are the zeros and the poles of OLTF? What are the zeros and the poles of CLTF? d. Write the algebraic relation between the error E(s)=R-Y and the reference R(s) in terms of G and K? Write it in the format E = some function of s * R. What is the TF from R to E? Write the algebraic relation between the controller output U(s) and the reference…
We consider a dynamical system represented by the block diagram: Simple negative feedback: U(s) E(s) input, + with T₁(s) T₂(s) = 2 = a 1+5² T,(s) T₂(s) X(S) output measurement with a 4 and Calculate the closed-loop transfer function at s=10.
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