5 Problem 4.41 Consider the second-order plant with transfer function: 1 G(s) = (s1)(5s 1) and...
Please answer all the questions with MATLAB and also upload the code. Thanks. 3 Experiment - Matlab controller complexity and steady-state 3.1 Consider the satellite-attitude control problem shown in following figure where the normalized parameters are J 10 spacecraft inertia; N-m-sec2 /rad erreference satellite attitude; rad actual satellite attitude; rad Hy 1 sensor scale; factor volts/rad Hr = 1 reference sensor scale factor ; volts/rad w= disturbance torque: N-m H, D(s) Js Figure 4: Satellite attitude control Suppose kP =...
Controller Plant 10s+5 (s+.8)(s--1) DAG) A feedback control system is shown in Figure 4.48 (a) Determine the system Type with respect to the reference input. (b) Compute the steady-state tracking errors for unit step and ramp inputs (e) Determine the system Type with respect to the disturbance input, w (d) Compute the steady-state errors for unit step and ramp đisturbance inputs 4.30
5. Consider a plant given by G()+2(s+1 in a un (s+2)(2s+1) 1n a unity feedback structure. (a) Determine the system type and the steady state error with respect to a tracking polynomial reference input with a proportional controller, D(s)5. (b) Verify your result using MATLAB by plotting unit step and ramp responses. Use the Matlab command 1sim() for ramp input. Attach the code and the plots. 5. Consider a plant given by G()+2(s+1 in a un (s+2)(2s+1) 1n a unity...
A second-order process is described by its transfer function G(s) = (s+1)(843) and a PI controller by Consider feedback control with unit feedback gain as shown in Figure 1 A disturbance D(s) exists, and to achieve zero steady-state error, a small integral component is applied. Technical limitations restrict the controller gain kp to values of 0.2 or less. The goal is to examine the influence of the controller parameter k on the dynamic response. D(s) Controller Process X(s) Y(s) Figure...
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...
[7] Sketch the root locus for the unity feedback system whose open loop transfer function is K G(s) Draw the root locus of the system with the gain Kas a variable. s(s+4) (s2+4s+20) Determine asymptotes, centroid, breakaway point, angle of departure, and the gain at which root locus crosses ja-axis. A control system with type-0 process and a PID controller is shown below. Design the [8 parameters of the PID controller so that the following specifications are satisfied. =100 a)...
Consider a mass-spring-damper system (i.e., the plant) described by the following second-order differential equation where y represents the position displacement of the mass. Our goal is to design a controller so that y can track a reference position r. The tracking error signal is then et)(t). (a) Let there be a PID controller Derive the closed-loop system equation in forms of ODE (b) Draw the block diagram of the whole system using transfer function for the blocks of plant and...
Consider a unity-feedback control system with a PI controller Gpr(s) and a plant G(s) in cascade. In particular, the plant transfer function is given as 2. G(s) = s+4, and the PI controller transfer function is of the forrm KI p and Ki are the proportional and integral controller gains, respectively where K Design numerical values for Kp and Ki such that the closed-loop control system has a step- response settling time T, 0.5 seconds with a damping ratio of...
5. A robotic arm is described by the first order transfer function G(s)A where Kp-1, however it may change with respect to the arm's position. (a) Design a control system that will reject a disturbance signal d(t)=3+3cos(t-r) without steady-state error. All desired closed-loop poles are positioned at-λ where-λ= 1. (b) In order to guarantee the closed-loop stability for the variation of Kp the maximum and minimum values of Kp 1 need to be determined. Use Routh- Hurwitz stability criterion to...
4.35 Consider the feedback control system with the plant transfer function G(s) = (5+0.1)(5+0.5) (a) Design a proportional controller so the closed-loop system has damping of 5 = 0.707. Under what conditions on kp is the closed-loop system stable? (b) Design a PI controller so that the closed-loop system has no over- shoot. Under what conditions on (kp, kt) is the closed-loop system is stable? (©) Design a PID controller such that the settling time is less than 1.7 sec.