SOLUTION MANUAL FOR CONTROL SYSTEMS ENGINEERING,
8TH EDITION BY NORMAN S. NISE || LATEST EDITION
, 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 ToThe 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 BeImplemented 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. TheSystem Will Either Destroy Itself, Reach An Equilibrium State Because Of
Saturation In Driving Amplifiers, Or Hit Limit Stops.
11. Natural Response
12. Determine The Transient Response Performance Of The System.
13. Determine System Parameters To Meet The Transient Response Specifications For The System.
14. True
15. Transfer Function, State-Space, Differential Equations
16. Transfer Function - The Laplace Transform Of The Differential Equation
State-Space - Representation Of An Nth Order Differential Equation As N Simultaneous
First-OrderDifferential Equations
Differential Equation - Modeling A System With Its Differential Equation
SOLUTIONS TO PROBLEMS
50 Volts
1. Five Turns Yields 50 V. Therefore K = = 1.59
5 X 2
Rad
,1-2 Chapter 1: Introduction
2.
Desired Temperature Voltage Actual
Fuel
Temperatur Difference Differenc Temperatur
Flow
e e e
Amplifier and Heater
+ valves
Thermostat
-
3.
Desired Input Error Aileron Roll Roll
Roll Voltag Voltag Position Rat Angle
Angle e e e
+ Aileron Aircraft
Pilot Integrate
Position Dynamics
controls
Control
-
Gyro
Gyro Voltage
4.
Input
Speed
Desired Voltag Actual
Error Motor
Speed e Spee
Voltag and
transducer Amplifier d
+ e drive
system
-
Dancer
Dancer
position
Voltage sensor dynamics
Proportiona
l
To Actual Speed
, 1-3 Solutions To Problems
5.
Input Power Rod
Voltag Error Position
Desired e Voltag Motor Actual
Power e and Power
+ Amplifier
Transducer drive Reactor
system
-
Sensor &
Voltage transducer
Proportiona
l
To Actual Power
6.
Graduating
And
Drop-
Out
Desired Actual
Rate
Desired Population Studen Actual Studen
t Net t
Rate
Student Error Rate Student - Of
Influx
Population
Population + Administration Admissions
Rate +
Integrate
-
7.
Voltage Voltage
Proportional Representing
To Desired Volume Actual Volume Actual
Desired Volume Volume
Error
Volume + Volume
Transducer Radio
control circuit
-
Effective
Volume
+
Voltage
- Proportional
To Speed
Transducer
-
Speed
8TH EDITION BY NORMAN S. NISE || LATEST EDITION
, 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 ToThe 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 BeImplemented 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. TheSystem Will Either Destroy Itself, Reach An Equilibrium State Because Of
Saturation In Driving Amplifiers, Or Hit Limit Stops.
11. Natural Response
12. Determine The Transient Response Performance Of The System.
13. Determine System Parameters To Meet The Transient Response Specifications For The System.
14. True
15. Transfer Function, State-Space, Differential Equations
16. Transfer Function - The Laplace Transform Of The Differential Equation
State-Space - Representation Of An Nth Order Differential Equation As N Simultaneous
First-OrderDifferential Equations
Differential Equation - Modeling A System With Its Differential Equation
SOLUTIONS TO PROBLEMS
50 Volts
1. Five Turns Yields 50 V. Therefore K = = 1.59
5 X 2
Rad
,1-2 Chapter 1: Introduction
2.
Desired Temperature Voltage Actual
Fuel
Temperatur Difference Differenc Temperatur
Flow
e e e
Amplifier and Heater
+ valves
Thermostat
-
3.
Desired Input Error Aileron Roll Roll
Roll Voltag Voltag Position Rat Angle
Angle e e e
+ Aileron Aircraft
Pilot Integrate
Position Dynamics
controls
Control
-
Gyro
Gyro Voltage
4.
Input
Speed
Desired Voltag Actual
Error Motor
Speed e Spee
Voltag and
transducer Amplifier d
+ e drive
system
-
Dancer
Dancer
position
Voltage sensor dynamics
Proportiona
l
To Actual Speed
, 1-3 Solutions To Problems
5.
Input Power Rod
Voltag Error Position
Desired e Voltag Motor Actual
Power e and Power
+ Amplifier
Transducer drive Reactor
system
-
Sensor &
Voltage transducer
Proportiona
l
To Actual Power
6.
Graduating
And
Drop-
Out
Desired Actual
Rate
Desired Population Studen Actual Studen
t Net t
Rate
Student Error Rate Student - Of
Influx
Population
Population + Administration Admissions
Rate +
Integrate
-
7.
Voltage Voltage
Proportional Representing
To Desired Volume Actual Volume Actual
Desired Volume Volume
Error
Volume + Volume
Transducer Radio
control circuit
-
Effective
Volume
+
Voltage
- Proportional
To Speed
Transducer
-
Speed
