The Class Name is: MAE 318 System Dynamics and Control I
Problem 1: Steady-state error analvsis (a) A block diagram of a feedback control system is given ...
Problem 51: (25 points) Figure 5 is an example of a feedback control system that is designed to regulate the angular position θ(t) of a motor shaft to a desired value θr(t). The signal e(t) represents the error between the measured shaft angle θ(t) and the desired shaft angle θ (t). The Laplace transforms ofa,(t), θ(t), and e(t) are denoted as ΘR(s), θ(s), and E(s), respectively. The control gains Ki and K2 are chosen by the control engineer to achieve...
For the feedback control system shown to the right: Find the steady state error with respect to the reference input and the disturbance for step, ramp, and parabolic inputs. Assume the inputs are 2s2 +3s+3 Equation Input Ste Ramp Parabolic H(s) = 1 r(t) = w(t) = 4t2 a. find the error to a step, ramp and parabolic input (reference input) b. find the error to a step. ramp and parabolic input (disturbance input)
pleas show all work thank you Disturbance D(s) Reference Control Output Input Error Input t US) Y(s) Plant Given the above closed loop block diagram: Let aundl s) KK (a) Show that the above system will have zero steady state error for step reference input (when D(s)-0) as well as for step disturbance input (when R(s)-0). (b) LetJ B K1 and Kp0, what about the stability of the closed loop system? Disturbance D(s) Reference Control Output Input Error Input t...
Consider the closed loop system defined by the following block diagram. a) Compute the transfer function E(s)/R(s). b) Determine the steady state error for a unit-step 1. Controller ant Itly Ro- +- HI- 4단Toy , c) d) e) reference input signal. Determine the steady state error response for a unit-ramp reference input signal. Determine the locations of the closed loop poles of the system. Select system parameters kp and ki in terms of k so that damping coefficient V2/2 and...
2. A feedback control system is subject to disturbances at the actuator input, as shown in the following block diagram. Remember that you need to use the final value theorem (and not the table) when dealing with any other input other than the reference. See the last 3 pages, 12-15, of my steady-state error lecture notes for examples on how to deal with disturbance rather than reference inputs D(s) 1 Y(s) $3+2s2+2s If the reference command is r(t) 1S 0,...
Consider the closed loop systema) Design a PD controller (that is, calculate K1 and K2) such that the system isstable and the steady-state error for the input r (t) = unity ramp letless than or equal to 0.02.b) Select a value from K1 and K2 and build the model in Simulink or solutionanalytical to obtain the response of the system to the magnitude rampr (t) = 2t.c) Graph the answer
A unity feedback system is shown in Fig. 1. The closed-loop transfer function ?(?) of this system is given as ?(?)=?1?4+2?3+(?2+1)?2+?2?+?1. a) (20%) Using Routh-Hurwitz criteria, find expression (in terms of ?1 and ?2) and range of value of ?1 and ?2 such that the above system is stable. b) (4%) It is desired to achieve steady-state error of less than 0.3 with a unit ramp input. Find an additional constrain in terms of ?1 and ?2 such that the...
Spring 2019 3. Given a closed-loop control system with unity feedback is shown in the block diagram. G(s) is the open-loop transfer function, and the controller is a gain, K. 1. (20) Calculate the open-loop transfer function tar →Q--t G(s) (10) Calculate the steady-state error to a step input of the open-loop system. 7. (in Bode Form) from the Bode plot. (10) Calculate the shortest possible settling time with a percentage overshoot of 5% or less. 8. 2. (10)Plot the...
Find the steady state error constants and the steady-state error response for the digital control system shown below, if the inputs are: a. Unit Step, u(t) b. Unit Ramp, t u(t) c. Unit Parabola, 0.5t2u(t) 2. R(s) + C(s) s(s 2) T=0.1
5, (29%) Consider the feedback control system in Figure-5 in block diagram form. The reference input R(s), system output Y(s), and disturbance D(s) are denoted along with the error E(s) and control effort F(s). You will design the control law Gc(s) to achieve certain performance criteria. Answer the following questions (assume D(s)0 in all parts except part(ü) (a) [396] Show that the transfer function relating the reference R(s) to the output Y(s) is given by (b) [3%) Assuming a proportional...