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Problem 6: The step response of a given system is 3 2 6...
control systems problem please help #6 (4 pts.) The unit-ramp response of a system is given...
control systems problem please help
#6 (4 pts.) The unit-ramp response of a system is given as follow, without applying LT find all closed loop poles.
Manually plot the unit step response of the following system Please include detailed step. 3. to...
Manually plot the unit step response of the following system Please include detailed step. 3. to you best knowledge. G(s)- Hint: You can use partial fraction expansion and inverse Laplace Transfer to find the unit step response. Please note that there is no damping term in this system and the system will oscillate at a constant maximum magnitude without decaying.
QUESTION 2 Given that a control system has a forward path of G(s) and negative unity...
QUESTION 2 Given that a control system has a forward path of G(s) and negative unity feedback and unit- step input is applied to the system. If G(s) is given as: K G(s)= s(s4) Draw the block diagram of the system. a) Derive the closed-loop transfer function of the system. b) If the gain K 6, determine the settling time of the resulting second-order system at 2% c) tolerance band Its corresponding steady state error. d) Sketch the controlled output...
Higher Colleges of Technology Faculty of Electronic Engineering Class Assignment 4 Second Order Systems EEC 4043:...
Higher Colleges of Technology Faculty of Electronic Engineering Class Assignment 4 Second Order Systems EEC 4043: Control Systems Score from 5 Student Name Student ID # You are required to analyze a DC motor speed control system shown in Figure I and 2 below. Figure 1 shows the equivalent circuit diagram of the DC motor control system, while Figure 2 shows the block diagram of the system feedback control G(s) drmanvee Motor Figare 2: The System Feedhack syacm daprams Figue...
Q4. 1 2 3 G 10 pts. Use MATLAB and plot the step response of the following systems G3 2s+1 figure. Gy on the same 2s+1...
Q4. 1 2 3 G 10 pts. Use MATLAB and plot the step response of the following systems G3 2s+1 figure. Gy on the same 2s+1 2s+1 Explain the similarities (at least 1) and differences (at least 1) between these responses. E_ figure. G, G 3 10 pts. Use MATLAB and plot the impulse response of the following systems Explain the similarities and differences between these responses. on the same 25+1 10 pts. Find the time constant (Te), pole(s), DC...
A control syste n whose response is step response,-0.60+ e") cascade to another control block whose...
A control syste n whose response is step response,-0.60+ e") cascade to another control block whose response is impulse response, e. What is the transfer function of the cascade system? a) (s-3)(s-2)) b) (s+3) (s +2) (s-3)(s-2) 1.8 d) (s +3)(s+2)
Problem 6 Model Parameters from the Transient Response The step input r(t) = Rous(t) (R(8) =...
Problem 6 Model Parameters from the Transient Response The step input r(t) = Rous(t) (R(8) = Ro/s) is applied to a system whose block diagram model is given below in Figure 8.24. The corresponding step response measurement is shown in Figure 8.25. In the sten response measurement, note that peak time is to = - ( 1.96) and the peak value is ctp) = 2.2. The open-loop transfer function G(s) is of the form $(8 + a) where a and...
(ENGINEERING SIGNALS AND SYSTEMS) MATLAB CODING: Project Description For this system for an unstable system You...
(ENGINEERING SIGNALS AND SYSTEMS)
MATLAB CODING:
Project Description For this system for an unstable system You will use MATLAB to perform most of your calculations and MATLAB code and a typewritten report documenting your results. project, you will design and simulate a feedback control You will submit a copy of your Background A block diagram of a system in the open loop and closed (feedback) loop configurations is given in Figure 1. Note that this feedback loop is different from...
Problem 1: Consider the block functional diagram of the satellite attitude control system shown in Figure...
Problem 1: Consider the block functional diagram of the satellite attitude control system shown in Figure (a), here below. The output of this system exhibits continued oscillations and is not desirable. This system can be improved by using a tachometer feedback. Ki, as shown in Figure (b). Assuming that = 4, using block diagram algebra and theory of time performance specifications for second order systems, please, compute: (1) the value of the gain K such that closed loop transfer function...
9. A control system is given by the following state-space representation -8 101 [2 dt 1-6 00 y [1...
this problem needs to be done using SciLab
9. A control system is given by the following state-space representation -8 101 [2 dt 1-6 00 y [1 0 0]x Please do the following: a. Find its transfer function representation. b. Calculate its zeros and poles c. Write a Scilab program to draw the step response and impulse response graphs in the same window with the step response graph in the upper half the window and the impuise response graph in...
control systems problem please help
#6 (4 pts.) The unit-ramp response of a system is given as follow, without applying LT find all closed loop poles.
Manually plot the unit step response of the following system Please include detailed step. 3. to you best knowledge. G(s)- Hint: You can use partial fraction expansion and inverse Laplace Transfer to find the unit step response. Please note that there is no damping term in this system and the system will oscillate at a constant maximum magnitude without decaying.
QUESTION 2 Given that a control system has a forward path of G(s) and negative unity feedback and unit- step input is applied to the system. If G(s) is given as: K G(s)= s(s4) Draw the block diagram of the system. a) Derive the closed-loop transfer function of the system. b) If the gain K 6, determine the settling time of the resulting second-order system at 2% c) tolerance band Its corresponding steady state error. d) Sketch the controlled output...
Higher Colleges of Technology Faculty of Electronic Engineering Class Assignment 4 Second Order Systems EEC 4043: Control Systems Score from 5 Student Name Student ID # You are required to analyze a DC motor speed control system shown in Figure I and 2 below. Figure 1 shows the equivalent circuit diagram of the DC motor control system, while Figure 2 shows the block diagram of the system feedback control G(s) drmanvee Motor Figare 2: The System Feedhack syacm daprams Figue...
Q4. 1 2 3 G 10 pts. Use MATLAB and plot the step response of the following systems G3 2s+1 figure. Gy on the same 2s+1 2s+1 Explain the similarities (at least 1) and differences (at least 1) between these responses. E_ figure. G, G 3 10 pts. Use MATLAB and plot the impulse response of the following systems Explain the similarities and differences between these responses. on the same 25+1 10 pts. Find the time constant (Te), pole(s), DC...
A control syste n whose response is step response,-0.60+ e") cascade to another control block whose response is impulse response, e. What is the transfer function of the cascade system? a) (s-3)(s-2)) b) (s+3) (s +2) (s-3)(s-2) 1.8 d) (s +3)(s+2)
Problem 6 Model Parameters from the Transient Response The step input r(t) = Rous(t) (R(8) = Ro/s) is applied to a system whose block diagram model is given below in Figure 8.24. The corresponding step response measurement is shown in Figure 8.25. In the sten response measurement, note that peak time is to = - ( 1.96) and the peak value is ctp) = 2.2. The open-loop transfer function G(s) is of the form $(8 + a) where a and...
(ENGINEERING SIGNALS AND SYSTEMS)
MATLAB CODING:
Project Description For this system for an unstable system You will use MATLAB to perform most of your calculations and MATLAB code and a typewritten report documenting your results. project, you will design and simulate a feedback control You will submit a copy of your Background A block diagram of a system in the open loop and closed (feedback) loop configurations is given in Figure 1. Note that this feedback loop is different from...
Problem 1: Consider the block functional diagram of the satellite attitude control system shown in Figure (a), here below. The output of this system exhibits continued oscillations and is not desirable. This system can be improved by using a tachometer feedback. Ki, as shown in Figure (b). Assuming that = 4, using block diagram algebra and theory of time performance specifications for second order systems, please, compute: (1) the value of the gain K such that closed loop transfer function...
this problem needs to be done using SciLab
9. A control system is given by the following state-space representation -8 101 [2 dt 1-6 00 y [1 0 0]x Please do the following: a. Find its transfer function representation. b. Calculate its zeros and poles c. Write a Scilab program to draw the step response and impulse response graphs in the same window with the step response graph in the upper half the window and the impuise response graph in...
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