Question

In addition to the transient response charactcristics considered above, we are often interested in tho steady-state response

Pre-Lab Question 10 (3 marks) What is the steady-state error in response to a step input R(s) in the presence of a constant d

will leave positive reviews

previous questions

0 0
Add a comment Improve this question Transcribed image text
Answer #1

ua haue and anj Con t GH 2 andA-Y ナ ftk DLS)- S) AYP 6) lo ト) Ds tpAś 4-1

Add a comment
Know the answer?
Add Answer to:
will leave positive reviews previous questions In addition to the transient response charactcristics considered above, we...
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
  • Use the Engineering approach to find the following (assuming: given): a) derive the zero-input r...

    Use the Engineering approach to find the following (assuming: given): a) derive the zero-input response of the circuit, b) derive the impulse response of the circuit, and c) derive the zero-state response to a step input (You are required to perform convolution by using the graphical method on this part). Draw the s-domain circuit (use a current source for the capacitor initial condition) for the circuit and perform s-domain analysis to find the following (assuming: given): a) zero-input response of...

  • Question 4: Consider the following system: 0.01 a) Describe the response to a unit step input...

    Question 4: Consider the following system: 0.01 a) Describe the response to a unit step input for K 0.01 and K-0.1 and determine the value of K for a non-oscillatory minimum response time. b) If we let K-1, what will be the value of the steady state error of this system in response to a unit step input? c) If we now replace the "proportional controller" (the box with the K in it) with a proportional integral (PI) controller, with...

  • Figure below shows the time response of the system mechanical figure above to a force in step of 8.5 N. Following the...

    Figure below shows the time response of the system mechanical figure above to a force in step of 8.5 N. Following the analysis of the system in the figure above a) Determine the transfer function X(s)/F(s) of the system and give the standard form of the latter. b) Based on the response of this system at 8.5 N, determine the , and parameters of the mechanical system. c) By combining the results found previously, determine the value of the three...

  • Q-7      The inlet temperature Ti(t) is a process disturbance and the he...

    Q-7      The inlet temperature Ti(t) is a process disturbance and the heater Q(s) is adjusted to maintain the outlet temperatureT(t) at a specified set point. Start with the following energy balance and find T(s)/Ti(s) and T(s)/Q(s) Determine if the two transfer functions are combined in parallel (additive) or series (multiplicative) and input the transfer functions in the appropriate boxes. Transfer Functions in Parallel: Transfer function in series: Show how the two transfer functions T(s)Ti(s) and T(s)Q(s) would fit into an...

  • Tutorial -On PID control (Control System: Instructor slides and lab) Consider a second order mass...

    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...

  • QUESTION 3 An L-shaped rigid bar is attached with a pivot to a wall as shown...

    QUESTION 3 An L-shaped rigid bar is attached with a pivot to a wall as shown in the figure below. Assume that the L-shaped rigid bar is massless. A mass of m = 9.1958 kg is attached to one end of the rigid bar and the other end is supported by spring k = 965.7083 N/m and damper c = 121.3183 Ns/m. Determinate the steady state amplitude of mass m, given where F0 =417.8427 N, ω = 48.0443 rad/s, and...

  • % We can couple the design of gain on the root locus with a % step-response...

    % We can couple the design of gain on the root locus with a % step-response simulation for the gain selected. We introduce the command % rlocus(G,K), which allows us to specify the range of gain, K, for plotting the root % locus. This command will help us smooth the usual root locus plot by equivalently % specifying more points via the argument, K. Notice that the first root locus % plotted without the argument K is not smooth. We...

  • You will look at both 1st and 2nd order approaches as you perform your analysis. Use math lab and Simulink as needed. Please show all calculations and any other means of analysis / simulation for full...

    You will look at both 1st and 2nd order approaches as you perform your analysis. Use math lab and Simulink as needed. Please show all calculations and any other means of analysis / simulation for full credit. Question three is the one needed to be solved, but 2 is needed to solve 3. Question 2) (25 points) Suppose instead of the cooling chamber modeled as a 1t order system, that the chamber was modeled as a 2nd system due to...

  • Consider the plant sDs2) 1) What is the plant's type? 2) Let C(s) - K (a...

    Consider the plant sDs2) 1) What is the plant's type? 2) Let C(s) - K (a proportional controller). Find the closed-loop transfer function from reference to output using unity feedback. ) Choose different gains for K within the range 1 to 100. Plot the unit step response for the different gains. What happens with the transient response of the closed-loop as K increases? 4) For K 20 find the maximum value attained by the output y(t) and the settling time...

  • 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...

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
ADVERTISEMENT