Example 3:Find the transfer function of the diagram shown below, which contain of amotor coupled to an inertial load through a shaft with a spring constant K. Anon-rigid coupling between two mechanical components in a controlsystem often causes torsional resonances that can be transmitted to all partsof the system.MOTORJm BmmKOmK0₁.LOADJL

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Answered: Find the transfer function of the…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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For the systems illustrated below, ﬁnd the natural frequencies, mode shapes and general responses for a mass and a pulley. The pulley has mass 2m and can be considered as a solid disk.
Find the Transfer Function G(s)= X3(s) / F(s) for each network shown in figure N°5 c
OBLEM 4. Using the condition (3.027) of Lect. 16, prove that the mo- mentum operator p is Hermitian. HINT: Use the periodic boundary conditions for the functions g(r) and s(x).
Figure 1 shows an electrical system comprising a series RLC circuit and input voltagesource ein(t).(a) Derive the input-output equation with output y = I and input u = ein(t). (b) Using the derived input-output equation, drive the system transfer function G(s)that relates output to input. Use the following numerical values for the electrical systemparameters: resistance R = 2Ω, inductance L = 0.25H, and capacitance C = 0.4F. (c) Using the derived transfer function, derive the time-domain ordinary differentialequation for the input-output equation of this electrical system. (d) Draw the complete block diagram of this series RLC circuit using the derived transferfunction.
A planer mechanism has 6 links with 6 lower pairs and 2 higher pairs. Then the degree of freedom of mechanism as per Gruebler's Criterion is
One of the tail rotor blades of a helicopter was damaged, and due to the repair, there is an extra 2 kg mass 0.40 m from the axis of rotation. The equivalent system before the repair had a mass of 102 kg and stiffness of 93.8 kN/m. Assume the rotor was well-balanced before the damage. The repaired helicopter tail has a damping ratio of 0.15. Find the steady-state response of the tail when the blades rotate at 1500 rpm.
It is observed from the magnitude plot of a compliance transfer function of a mass spring damper that the value at a very small frequency 0.0001 is 3.71 meters and at resonance 1.10 rad/s is 7.10 meters. What is the natural frequency, damping coefficient, stiffness, and mass of the system?
Obtain the transfer function of the operational-amplifier circuit shown in Figure 3–28
Suppose a spring mass damper system with k=4000N/m, m=10kg,and c=40N-s/m Find the steady-state and total response of the system under harmonic force F(t)=200 cos t N and the initial conditions x0=0.1m and ̇x0'=0
1. Determine the driven response for: Bi k B2 k mi m2 Given: ID k spring constant, mě – mass, B: - damping coefficient, F(t) Initial data: ID = 500351 ID % 4 = 1

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