Matlab control
The open-loop system dynamics model for the NASA eight-axis Advanced Research Manipulator II (ARM II) electromechanical shoulder joint/link, actuated by an armature-controlled dc servomotor is shown in Figure P1.
The ARM II shoulder joint constant parameters are
Ka= 12, L=0.006 H, R= 1.4 Ω, Kb= 0.00867, n=200, Km= 4.375, J=Jm+ JL /n2, D=Dm+DL /n2, JL= 1, DL= 0.5, Jm= 0.00844, and Dm= 0.00013.
FIGURE P1 Open-loop model for ARM ll
(Due to 29/8/2020)
a. Obtain the equivalent open-loop transfer function, ?(?) (with a unity feedback system) (using MatLab or MatLab/Simulink).
b. The loop is to be closed by cascading a controller, Gc1(s) = KP, with G(s) in the forward path forming an equivalent forward-transfer function, Ge(s) = Gc1(s) G(s). Parameters of Gc1(s) will be used to design a desired transient performance. The input to the closed-loop system is a voltage, VI(s), representing the desired angular displacement of the robotic joint with a ratio of 1 volt equals 1 radian. The output of the closed-loop system is the actual angular displacement of the joint, θL(s). An encoder in the feedback path, Ke, converts the actual joint displacement to a voltage with a ratio of 1 radian equals 1 volt. Draw the closed loop system showing all transfer functions. (Use Microsoft PowerPoint or Visio to draw the system)
c. Find the closed-loop transfer function ?(?). (using MatLab or MatLab/Simulink).
d. Determine the range of KP for which the system is stable (using root locus technique).
e. Determine the step response for four different values of KP including stability and instability conditions (using MatLab or MatLab/Simulink).
f. Determine the transient parameters for a selected stable oscillatory response (rising time, settling time, overshoot (if exists) and compare and discuss the response (using MatLab or MatLab/Simulink). (choose a value for KP)
g. What is the min. steady state error of this system?
Homework Answers
It has to be answered using matlab and other programs as each section says
The open-loop system dynamics model for the NASA eight-axis Advanced Research Manipulator II (ARM II) electromechanical shoulder joint/link, actuated by an armature-controlled dc servomotor is shown in Figure P1.The ARM II shoulder joint constant parameters areKa= 12, L=0.006 H, R= 1.4 Ω, Kb= 0.00867, n=200, Km= 4.375, J=Jm+ JL /n2, D=Dm+DL /n2, JL= 1, DL= 0.5, Jm= 0.00844, and Dm= 0.00013.FIGURE P1 Open-loop model for ARM ll(Due to 29/8/2020)a. Obtain the equivalent open-loop transfer function, ?(?) (with a unity feedback...
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Control Lab
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Q2 (a) Consider the control system shown in Figure Q1 (a). Obtain the closed-loop transfer function of this system and by using MATLAB obtain the unit step response of this closed loop system - R(S) c(s) 36+1) (s + 1) Figure Q2 (a) (b) A sampler and a zero-order hold element were inserted into the system in Figure Q1(a) as shown in Figure Q1(b). Obtain the closed-loop pulse transfer function of this system and by using MATLAB or otherwise, obtain...
7. For a negative feedback control system with unit feedback gain, its open-loop 100 transfer function...
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4) A unity feedback...
part 2 & part 3 please...
Tutorial -On PID control (Control System: Instructor slides and lab) Consider a second order mass-force system to study its behavior under various forms of PID control xtn fon force In Disturbance force: 50) (i.e. wind force) Part I (dealing with the plant/process) 1. What is the model of this system, in other words, write the ODE of the system 2. Derive the transfer function of the above system from Fls) to X(s) 3. What...
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7. For a negative feedback control system with unit feedback gain, its open-loop 100 transfer function is G (s) Design a PID controller, so that the open s(10s) corresponding closed-loop poles are -2+jl and -5. (10 scores)
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