CONTROL SYSTEMS ENGINEERING 7TH EDITION
BY NORMAN S. NISE SOLUTION MANUAL ||COMPLETE
GUIDE||GRADED A+
, O N E
Introduction
ANSWERS TO REVIEW QUESTIONS
1. Guided Missiles, Automatic Gain Control In Radio Receivers, Satellite Tracking Antenna
2. Yes - Power Gain, Remote Control, Parameter Conversion; No - Expense, Complexity
3. Motor, Low Pass Filter, Inertia Supported Between Two Bearings
4. Closed-Loop Systems Compensate For Disturbances By Measuring The Response, Comparing
It To The Input Response (The Desired Output), And Then Correcting The Output Response.
5. Under The Condition That The Feedback Element Is Other Than Unity
6. Actuating Signal
7. Multiple Subsystems Can Time Share The Controller. Any Adjustments To The Controller
Can Be Implemented With Simply Software Changes.
8. Stability, Transient Response, And Steady-State Error
9. Steady-State, Transient
10. It Follows A Growing Transient Response Until The Steady-State Response Is No Longer
Visible. The System Will Either Destroy Itself, Reach An Equilibrium State Because Of Saturation
In Driving Amplifiers, Or Hit Limit Stops.
11. Transient Response
12. True
13. Transfer Function, State-Space, Differential Equations
14. Transfer Function - The Laplace Transform Of The Differential Equation
State-Space - Representation Of An Nth Order Differential Equation As N Simultaneous First-
Order Differential Equations
Differential Equation - Modeling A System With Its Differential Equation
SOLUTIONS TO PROBLEMS
50
1. FIVE TURNS YIELDS 50 V. = 1.59
THEREFORE K =
VOLTS 5 X
2 RAD
,
, 2
C
2. h
DESIRED
a
TEMPERATUR VOLTAGE
FUEL ACTUAL
DIFFERENC
TEMPERATU
RE
+
E
p
DIFFERENCE E
FLOW TEMPERATURE
Amplifier and
-
t Thermostat valves
Heater
e
r
3.
1
:
AILERO
DESIRED
ROLL IINPUT
VOLTA
ERROR
VOLTA N
ROL
L
ROLL
ANGL
ANGLE GE GE POSITIO RAT E
controls
n + N E
t -
r
o
4.
d
u INPUT
VOLTA
SPEED
DESIRED ACTUA
SPEED
transducer
cGE
ERROR
VOLTA
Amplifier
Motor
and L
+ GE drive SPEED
t system
i - Dancer
position
Dancer
dynamics
o sensor
n VOLTAGE
PROPORTIO
NAL
TO ACTUAL SPEED
5.
INPUT POWE ROD
VOLTA R POSITIO
DESIRED GE ERROR Motor N ACTUA
power VOLTA and L
+ Amplifier
Transducer drive Reactor POWE
GE
system R
-
Sensor &
BY NORMAN S. NISE SOLUTION MANUAL ||COMPLETE
GUIDE||GRADED A+
, O N E
Introduction
ANSWERS TO REVIEW QUESTIONS
1. Guided Missiles, Automatic Gain Control In Radio Receivers, Satellite Tracking Antenna
2. Yes - Power Gain, Remote Control, Parameter Conversion; No - Expense, Complexity
3. Motor, Low Pass Filter, Inertia Supported Between Two Bearings
4. Closed-Loop Systems Compensate For Disturbances By Measuring The Response, Comparing
It To The Input Response (The Desired Output), And Then Correcting The Output Response.
5. Under The Condition That The Feedback Element Is Other Than Unity
6. Actuating Signal
7. Multiple Subsystems Can Time Share The Controller. Any Adjustments To The Controller
Can Be Implemented With Simply Software Changes.
8. Stability, Transient Response, And Steady-State Error
9. Steady-State, Transient
10. It Follows A Growing Transient Response Until The Steady-State Response Is No Longer
Visible. The System Will Either Destroy Itself, Reach An Equilibrium State Because Of Saturation
In Driving Amplifiers, Or Hit Limit Stops.
11. Transient Response
12. True
13. Transfer Function, State-Space, Differential Equations
14. Transfer Function - The Laplace Transform Of The Differential Equation
State-Space - Representation Of An Nth Order Differential Equation As N Simultaneous First-
Order Differential Equations
Differential Equation - Modeling A System With Its Differential Equation
SOLUTIONS TO PROBLEMS
50
1. FIVE TURNS YIELDS 50 V. = 1.59
THEREFORE K =
VOLTS 5 X
2 RAD
,
, 2
C
2. h
DESIRED
a
TEMPERATUR VOLTAGE
FUEL ACTUAL
DIFFERENC
TEMPERATU
RE
+
E
p
DIFFERENCE E
FLOW TEMPERATURE
Amplifier and
-
t Thermostat valves
Heater
e
r
3.
1
:
AILERO
DESIRED
ROLL IINPUT
VOLTA
ERROR
VOLTA N
ROL
L
ROLL
ANGL
ANGLE GE GE POSITIO RAT E
controls
n + N E
t -
r
o
4.
d
u INPUT
VOLTA
SPEED
DESIRED ACTUA
SPEED
transducer
cGE
ERROR
VOLTA
Amplifier
Motor
and L
+ GE drive SPEED
t system
i - Dancer
position
Dancer
dynamics
o sensor
n VOLTAGE
PROPORTIO
NAL
TO ACTUAL SPEED
5.
INPUT POWE ROD
VOLTA R POSITIO
DESIRED GE ERROR Motor N ACTUA
power VOLTA and L
+ Amplifier
Transducer drive Reactor POWE
GE
system R
-
Sensor &
