Question

5., A controller in Figure 4-18 is required to produce a steady-state output, do, that is within 2 percent of the commanded i
40 (2s + 1X5s +1) r(t)-5 u(t) c(t) Kc3(s+2)/(s+3)(S+1) Figure 4-18
0 0
Add a comment Improve this question Transcribed image text
Answer #1

3(s+2) C(s) R(S) @ks her contrtl therづウ 643H 3 (s) R(s) S13 (s+) Ris) proble m s E(5)| ラ|-o.kk» sE(s) < 0.1] 0-1 ウ | Am S-+0ak)t3 01415 15-ㅡ 스 0-1 --(M) Assuming tht the Value From (11) ,We have ke is-sitive → 01 ke-155/) 2 0.1 ke+3 Minimum urlue tfFor further help, please write in the comments.

Add a comment
Know the answer?
Add Answer to:
5., A controller in Figure 4-18 is required to produce a steady-state output, do, that is...
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for? Ask your own homework help question. Our experts will answer your question WITHIN MINUTES for Free.
Similar Homework Help Questions
  • The objective of the controller design in Fig. 1 is to find the controller Gc(s) such...

    The objective of the controller design in Fig. 1 is to find the controller Gc(s) such that I.)The closed-loop system is stable ii.)The output of the system above (y(t)) can track the reference input r(t) = At (A>0 is any real number). Use the Nyquist plot and Nyquist criterion to show that: a.)The portional controller Gc(s)=K can achieve asymptotic tracking of the ramp input r(t)=At but cannot meet the stability requirement for 0<K<+inf. b.) Can the PI controller Gc(s)=K(1+10/s) be...

  • 1. (15pts) Design a LEAD controller for the heading control of an antenna. The purpose of...

    1. (15pts) Design a LEAD controller for the heading control of an antenna. The purpose of this system is to have the azimuth angle output of the antenna, θ。(t), follow the input angle of the potentiometer, θ(t). Figure (a) shows a scheme of this system. Antesna Potentioneter 0i 8. K (s) G(s) Azimuth arglk Desised rimeth angle eput 6.625 Ts +1 G(s) = s(s +1.71) (s +100) The control objectives are: ·Steady state error of 12.9% for a unit-ramp input...

  • Problem 4) (20 Pts.) A Proportional controller is simply a gain block. In figure below, it...

    Problem 4) (20 Pts.) A Proportional controller is simply a gain block. In figure below, it is the block with gain 2nd order underdamped plant as shown. Kc which is behind the a) Simplify below block diagram to obtain the overall feedback system transfer funion)R(G) b) Choose Kc so that the overall feedback system transfer function G(s) has 50% overshoot due to a step input (called quarter decay ratio tuning) d) The feedback system transfer function Gs)- is faster than...

  • G) r(t) Figure 1: Feedback control system A pulley and belt transmission has a linearized relationship between the driven pulley angle θ(t) in degrees and the input torque u(t) in Newton meters given...

    G) r(t) Figure 1: Feedback control system A pulley and belt transmission has a linearized relationship between the driven pulley angle θ(t) in degrees and the input torque u(t) in Newton meters given by the following differential equation du(t) A feedback control system (illustrated in Figure 1) needs to be designed such that the closed-loop system is asymptotically stable and such that the following design criteria are met: 1. the gain crossover frequency a should be between and a 2....

  • 4) A unity feedback control system shown in Figure 2 has the following controller and process with the transfer functions: m(60100c Prs(s +10(s+7.5) a) Obtain the open- and closed-loop transfer f...

    4) A unity feedback control system shown in Figure 2 has the following controller and process with the transfer functions: m(60100c Prs(s +10(s+7.5) a) Obtain the open- and closed-loop transfer functions of the system. b) Obtain the stability conditions using the Routh-Hurwitz criterion. e) Setting by trial-and-error some values for Kp, Ki, and Ko, obtain the time response for minimum overshoot and minimum settling time by Matlab/Simulink. Y(s) R(s) E(s) Fig. 2: Unity feedback control system 4) A unity feedback...

  • Consider the aircraft model shown in Figure 1. We will assume that the aircraft is in steady-crui...

    Consider the aircraft model shown in Figure 1. We will assume that the aircraft is in steady-cruise at constant altitude and velocity; thus, the thrust, drag, weight and lift forces balance each other in the x- and y directions. We will also assume that a change in pitch angle will not change the speed of the aircraft under any circumstance (unrealistic but simplifies the problem a bit). Under these assumptions the longitudinal equations of motion for the aircraft can be...

  • The parameters are as follows k=10 a=0.50 b=0.3 c=0.6 d=9 w_1=12 w_2=15 Kv=30 A feedback control system (illustrated in Figure 1) needs to be designed such that the closed-loop system is asymptotical...

    The parameters are as follows k=10 a=0.50 b=0.3 c=0.6 d=9 w_1=12 w_2=15 Kv=30 A feedback control system (illustrated in Figure 1) needs to be designed such that the closed-loop system is asymptotically stable and such that the following design criteria are met: the gain crossover frequency wc should be between w1 and w2. the steady-state error should be zero in response to a unit step reference. the velocity constant should be greater than Kv (in other words, the steady-state unit...

  • control system System Description: The figure 1 and 2 below show, respectively, components and block diagram...

    control system System Description: The figure 1 and 2 below show, respectively, components and block diagram of a motor and the measurements of velocity (via the tacho unit) and position (via the potentiometer). n represents the gearbox ratio between the rotating shaft and the output shaft. The left-hand side of the diagram represents the controller. A reference set point for the rotating shaft is entered in degrees and this is equivalent voltage. The error is calculated by subtracting the measured...

  • A unity feedback closed loop control system is displayed in Figure 4. (a) Assume that the control...

    Please solve as a MATLAB code. A unity feedback closed loop control system is displayed in Figure 4. (a) Assume that the controller is given by G (s) 2. Based on the lsim function of MATLAB, calculate and obtain the graph of the response for (t) at. Here a 0.5°/s. Find the height error after 10 seconds, (b) In order to reduce the steady-state error, substitute G (s) with the following controller This is a Proportional-Integral (PI) controller. Repeat part...

  • Question 4 (a) A feedback control system with a proportional controller is shown in Figure Q4...

    Question 4 (a) A feedback control system with a proportional controller is shown in Figure Q4 (a). (i) Sketch the root locus of the system, (ii) Design the proportional controller (choose the value of K) such that the damping ratio does not exceed 0.5 and the time constant is less than 1 second. [All necessary steps of root locus construction and controller design must be shown). C(s) R(S) + s(s+4)(s + 10) Figure Q4 (a). A feedback control system [11...

ADVERTISEMENT
Free Homework Help App
Download From Google Play
Scan Your Homework
to Get Instant Free Answers
Need Online Homework Help?
Ask a Question
Get Answers For Free
Most questions answered within 3 hours.
ADVERTISEMENT
ADVERTISEMENT