System Dynamics
System Dynamics
3rd Edition
ISBN: 9780073398068
Author: III William J. Palm
Publisher: MCG
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Chapter 11, Problem 11.36P

The following equations are the model of the roll dynamics of a missile ([Bryson. 1975]). See Figure Pl 1.36.

Chapter 11, Problem 11.36P, The following equations are the model of the roll dynamics of a missile ([Bryson. 1975]). See Figure , example  1

Chapter 11, Problem 11.36P, The following equations are the model of the roll dynamics of a missile ([Bryson. 1975]). See Figure , example  2

where 5 = aileron deflection

b = aileron effectiveness constant

it = command signal to the aileron actuator

tp = roll angle, to = roll rate

Using the specific values b = 10s-1 and r = 1 s, and assuming that the state variables 5, to, and tp can be measured, develop a linear state-feedback controller to keep tp near 0. The dominant roots should be s = —10 ± 1 Oj, and the third root should be v = —20.

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A velocity of a vehicle is required to be controlled and maintained constant even if there are disturbances because of wind, or road surface variations. The forces that are applied on the vehicle are the engine force (u), damping/resistive force (b*v) that opposing the motion, and inertial force (m*a). A simplified model is shown in the free body diagram below. From the free body diagram, the ordinary differential equation of the vehicle is: m * dv(t)/ dt + bv(t) = u (t) Where: v (m/s) is the velocity of the vehicle, b [Ns/m] is the damping coefficient, m [kg] is the vehicle mass, u [N] is the engine force. Question: Assume that the vehicle initially starts from zero velocity and zero acceleration. Then, (Note that the velocity (v) is the output and the force (w) is the input to the system): 1. What is the order of this system?
A velocity of a vehicle is required to be controlled and maintained constant even if there are disturbances because of wind, or road surface variations. The forces that are applied on the vehicle are the engine force (u), damping/resistive force (b*v) that opposing the motion, and inertial force (m*a). A simplified model is shown in the free body diagram below. From the free body diagram, the ordinary differential equation of the vehicle is: m * dv(t)/ dt + bv(t) = u (t) Where: v (m/s) is the velocity of the vehicle, b [Ns/m] is the damping coefficient, m [kg] is the vehicle mass, u [N] is the engine force. Question: Assume that the vehicle initially starts from zero velocity and zero acceleration. Then, (Note that the velocity (v) is the output and the force (w) is the input to the system): A. Use Laplace transform of the differential equation to determine the transfer function of the system.
What is the step response of the dynamic system pictured below?
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