Please solve the following by hand and without the use of AI. Thank you! The feedback control system shown in Figure 4 is used to control the angularposition of a satellite dish. The desired angle, Bref, is set using a rotary dial. Km, T, and K, are systemparameters, constant and un-adjustable. Kp is the gain of the proportional controller (amplifier).Find the closed loop transfer functionFind the steady state error if the desired angle is 3 degrees. Determine theeffect of Kp.Replace the amplifier with a proportional-plus-integral (PI) controller and set Km = K = 1, t=0.5 for parts c) and d).Determine the gains of the controller that result in double poles of -0.25 for the closedloop system.Use half of the Kp found for part c) and determine the new K; and double poles. Commenton the effect of Kp on the pole locations.AmplifierMotor andMechanical LoadActualSatelitedish angleKΩᎾDesiredSatellite dishangleKp1+ TsSKsAngle SensorFigure 4 Feedback Control System for a satellite

Answered: The feedback control system shown in…

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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do not solve the last part ofthe question which states “Obtain the steady-state error when the disturbance qd is a unit-stepfunction”.
Please solve the following by hand and without the use of AI. Thank you!
The satallite system below is controlled using reaction wheels. The torque wheel input for the system is u(s) and the satallite attitude is Ө(s) For a strong communication link Ө needs to be a value where the satallite atenna is pointing at the ground station The transfer function for this system will be shown in the picture. Design a feedback control system that sets the closed loop damping ratio at 0.8 and the natural frequency is at 10 rad/sec.
1) Consider the system below: Vehicle Controller Steering dynamics Desired Actual bearing angle bearing angle 50 1 K s2 + 10s + 50 s(s + 5) Figure 1: Simplified Block Diagram of a Self-Guiding Vehicle's Bearing Angle Control. • Find a K value that the system has minimum rise time and minimum overshoot. Let us call this proportional gain as Kopt Show each step while finding Kopt- Show the necessary graphical solutions. Simulate the system response with 3 different K values. (Kopt and two other K values close to Kopt) Show the system response (actual bearing angle) in a single graph for different K values. • Comment on the results.
If the system is to be arranged in a closed-loop, with a controller gain K in the forward path and a unity negative feedback loop, what is the maximum value of K which could be used without the system becoming unstable? Assuming you use Figure Q5 for this, use a sketch to show how you obtained the values from the plot.
A feedback system is shown in the following figure Use Nyquist Criterion to determine the range of k that can make the system response stable. Discussion: if it is required that the system Maximum overshoot needs to be lower than 15%, would it be able to determine the k range without Bode diagram? if so, please briefly explain the general procedure of how you plan to find out k range; if not, please explain why. ( do not need to calculate for it, just explain the general procedure, or why it does not work)
Solve the following question by hand and without the use of AI. Use detailed mathematical expressions to solve the problem and please do not use AI. Thank You!
Figures 4: show a pneumatic controller. The pneumatic relay has the characteristic that pc=K pb , where K>0. What kind of control action does this controller produce? a. Derive the mathematical model for the system b. Derive the transfer function Pc(s)/E(s) -Solve step by step Orifice F+Ph R₁ Actuating error signal Flapper Nozzle. x+x F+Pe think
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The open loop transfer function of a unity feedback control system is given below; G(s) = K s(s+2)(s2+2s+2) Plot the root locus and determine the value of k at the break away point.
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R(s) C P 3. For the unity feedback system above, where Controller C = K Plant P = 1 Octave. a. s(s+4)(s+8) Plot the root locus b. Find the value of gain K for which the system is closed-loop stable. 4. Use pzmap function in Octave to get the pole zero map for the closed loop poles in the problem 3 with K=0,1,10,100,1000,10000, 100000. Submit code used to generate the transfer function and the pole-zero map figure for each system.

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