after row transformation we take the determinant
comparing the coefficient of both characteristic equation will
give the value of 'K' matrix
1) The following state-space system is dominated by a pair of lightly damped poles, 0 -1...
3. (20 pts.) Consider the system: where: C-1 0 0 -4 0 7 a) Analyze the stability of the system. b) Design a regulator for this system using the pole-placement with observer approach. Assume that the desired closed-loop poles for the pole placement part are located at: The desired observer poles are: S--7 c) Obtain the transfer function of the observer controller. S--7
3. Consider a system with the following state equation h(t)] [0 0 21 [X1(t) [x1(t) y(t) [0.1 0 0.1x2(t) X3(t) The unit step response is required to have a settling time of less than 2 seconds and a percent overshoot of less than 5%. In addition a zero steady-state error is needed. The goal is to design the state feedback control law in the form of u(t) Kx(t) + Gr(t) (a) Find the desired regon of the S-plane for two...
uestion 2 (25% total a) For a lightly-damped SDOF system, let x, and 1,- be the free vibration displacement amplitudes at the initial (reference) moment and m cycles later, respectively. (15%) In the class we concluded that the damping ratio can be estimated using logarithmic decrement as (LI) 27m Does this method still work if instead of displacement amplitudes, we use velocity amplitudes? That is, can be estimated based on 1+m where v, and Vi+ are the free vibration velocity...
1. Write the MATLAB commands (tf.) and zpk (...)) that yield the following trans fer functions: ii) Hy=1+1+ ii) H3-3-*+-1 (s + 1)( -2) iv) H. - 3)(8 + 4) 2. Consider the feedback system: C(0) = K * G(s) Determine the values of K, a, and b of C(s) such that the dominant-closed loop poles are located at $12 = -1 j. Use the root locus method. Provide the locations of the dominant poles. You should include the root...
Problem 2: Output-feedback stabilization Consider the following system 0 -8 3-3 4 [2-92]z y = a) Verify that the system is observable and controllable. Then, design an output-feedback controller (based on a full-order observer) by placing the poles of the closed loop system at -1 j, -3, 12 ±j2. and-30 (mention which desired poles you select for your observer design and why).
state space control
(d) Select K such that the closed-loop system poles are placed at s = 9 and s = 4. Problem 5: Consider the horizontal motion of a particle of u mass sliding under the influence of gravity on a frictionless wire. It can be shown that, if the wire is bent so that its height h is given by h(x)V(), then a state-space model for the motion is given by dr Suppose (a) Verify that the above...
5. For each of the following, determine if the system is underdamped, undamped, critically damped or overdamped ad sketch the it step response (a) G (s) = (c) G(s)-t 2+68+ (d) G (s) = 36 6. The equation of motion of a rotational mechanical system is given by where θ° and θί are respectively, output and input angular displace- ments. Assuming that all initial conditions are zero, determine (a) the transfer function model. (b) the natural frequency, w natural frequency,...
5. For each of the following, determine if the system is underdamped, undamped, critically damped or overdamped ad sketch the it step response (a) G (s) = (c) G(s)-t 2+68+ (d) G (s) = 36 6. The equation of motion of a rotational mechanical system is given by where θ° and θί are respectively, output and input angular displace- ments. Assuming that all initial conditions are zero, determine (a) the transfer function model. (b) the natural frequency, w natural frequency,...
Test 1 2: A state space representation of a system is given by: -2 011 y=[0 1]x 1. Design a state variable feedback control to place the closed-loop poles s =-3 ±j2. Assume that the complete state vector is available for feedback.。 Find the resulted close loop transfer function.
The transfer function of a linear system is G(s) = Y(s) S-1 U(s) 5? + 4s +3 a. Express this system in the modal form. b. Express this system in the standard controllable form (SCF). (Parts d, e, f, and g use this system) c. In the standard controllable form, suppose the output is replaced by y=[-1 a] | [x2] Give a value for a which makes the system unobservable. d. What is y(t) if y(0-)=-3, ay = 6 and...