Midterm Sample Problem - Transfer Function - Introduction to Controls | MEM 255, Exams of Mechanical Engineering

Material Type: Exam; Class: Introduction to Controls; Subject: Mechanical Engr & Mechanics; University: Drexel University; Term: Unknown 1989;

Typology: Exams

Pre 2010

Uploaded on 08/18/2009

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MEM 255 Midterm Sample Problems
1. For the system shown, determine:
a. The transfer function
(
)
(
)
Us Ys,
b. The impulse and step responses
()Us
()Ys
2
(4)s
+
2
2
s
s
+
(
)
()
32
6
s
s
+
+
2. Consider a system with transfer function
()
2
2
Gs s
=
+
a. Compute the response to the input
)
)
cosut t=,
b. Sketch the bode plot,
c. Repeat part a) for the transfer function
()
2
2
s
Gs s
=
+
3. Consider a dc motor driving a mechanical load, similar to an antenna positioning
servo. The equations of motion are:
()
(
)
() () () ()
() ()
() () ()
2
2
bB
a
aa a b a
mTa
m
dt
vt K dt
di t
R
it L vt vt
dt
Tt Kit
dt dt
JCTt
dt dt
θ
θθ
=
++=
=
+=
Construct the state equations where the applied armature voltage is the input,
and the angular position is the output.
()
a
vt
()
t
θ
pf3

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MEM 255 Midterm Sample Problems

  1. For the system shown, determine:

a. The transfer function U ( s ) → Y ( s ),

b. The impulse and step responses

U s ( ) (^) Y s ( )

2 ( s +4)

2 2

s s +

3 2 6

s s

  1. Consider a system with transfer function

G s s

a. Compute the response to the input u t ( ) = cos( t ),

b. Sketch the bode plot, c. Repeat part a) for the transfer function

s G s s

  1. Consider a dc motor driving a mechanical load, similar to an antenna positioning servo. The equations of motion are:

2 2

b B

a a a a b a

m T a

m

d t v t K dt di t R i t L v t v t dt T t K i t d t d t J C T t dt dt

Construct the state equations where the applied armature voltage is the input, and the angular position is the output.

va ( ) t

θ ( ) t

Nomenclature v b Motor back emf i a Armature current v a Armature voltage

θ Load angular position

T m Mechanical torque R a Armature resistance L a Armature inductance K (^) B Motor back emf coefficient K (^) T Motor torque coefficient J Motor & load inertia C Friction constant

  1. Using the partial fraction expansion method compute the step input response of the system shown below. U ( s ) Y ( s ) 2 12 1 7 12

s s s

  1. Consider the ship shown. A model used to study the yaw dynamics for a variety of stable and unstable ships is

T T 1 2 ψ ^ + ( T 1 + T 2 ) ψ + ψ = K ( δ + T 3 δ)

where the parameters are determined

for each specific ship. Determine state variable and a transfer function models that relate the output

T T 1 , 2 (^) , T 3 , K

ψ to the input δ.

  1. Find the transfer function for a system described by the state space model:

[ ] =[ ]

0 0 1 1 1 0 0 , 0 , 1 1 1 , 0 0 1 0 0

A b c d

⎡ −⎤ ⎡ ⎤ = ⎢^ ⎥^ = ⎢ ⎥ = ⎢ ⎥ ⎢ ⎥ ⎢⎣ ⎥⎦ ⎢ ⎥⎣ ⎦

V , velocity

, heading

β , sideslip

ψ

δ , rudder

  1. Consider the magnetically suspended ball shown below. An equilibrium voltage V

maintains a current that induces a magnetic field sufficient to hold the ball at a gap

. The linearized equations governing the motion of the ball are:

eq i eq h eq