Solution Manual for Control Systems Engineering, 8th Edition by Norman S. Nise |All Chapters |Complete guide A+.

, 1-17 Solutionsto v i vi


Problems
vi




ON E

Introduction
ANSWERSTOREVIEWQUESTIONS vi vi vi




1. Guided missiles, automatic gain control in radio receivers, satellite tracking antenna
vi vi vi vi vi vi vi vi vi vi




2. Yes - power gain, remote control, parameter conversion; No - Expense, complexity
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3. Motor, low pass filter, inertia supported between two bearings
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4. Closed-loop systems compensate for disturbances by measuring the response, comparing it
vi vi vi vi vi vi vi vi vi vi




tothe input response (the desired output), and then correcting the output response.
vi vi vi vi vi vi vi vi vi vi vi vi vi




5. Under the condition that the feedback element is other than unity
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6. Actuating signal vi




7. Multiple subsystems can time share the controller. Any adjustments to the controller can
vi vi vi vi vi vi vi vi vi vi vi vi




vi beimplemented with simply software changes.
vi vi vi vi vi




8. Stability, transient response, and steady-state error
vi vi vi vi vi




9. Steady-state, transient vi




10. It follows a growing transient response until the steady-state response is no longer visible.
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vi Thesystem will either destroy itself, reach an equilibrium state because of saturation in driving
vi vi vi vi vi vi vi vi vi vi vi vi vi vi




vi amplifiers, or hit limit stops. vi vi vi vi




11. Natural response vi




12. Determine the transient response performance of the system. vi vi vi vi vi vi vi




13. Determine system parameters to meet the transient response specifications for the system.
vi vi vi vi vi vi vi vi vi vi vi




14. True
15. Transfer function, state-space, differential equations
vi vi vi vi




16. Transfer function - the Laplace transform of the differential equation
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State-space - representation of an nth order differential equation as n simultaneous first-
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orderdifferential equations
vi vi




Differential equation - Modeling a system with its differential equation
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v i rad



SOLUTIONS TO PROBLEMS vi vi




50 volts vi

1. Five turns yields 50 v. Therefore K =
5 x 2 
vi vi vi vi vi vi vi


vi vi vi

,= 1.59
vi

, 1-2 v i Chapter 1: vi v i Introduction




2.


Desired Temperature Voltage Actual
vi
Fuelflo
vi

temperatur difference differenc
vi
temperatur
vi
w vi


e e e
Amplifier
vi
Heater
+ vi Thermostat andvalv
vi vi vi


es
-


3.


Desired vi Input Error Aileronvi Roll vi Roll
roll voltag
vi voltag
vi position rate angl
vi


angle e e e
vi vi vi vi vi vi vi vi vi


vi Pilot vi
+
vi vi
Ailero Aircraft
Integrate
vi controls n positio
vi
dynamic
vi


s
- n contro
vi


l


Gyro
Gyro voltage vi




4.
Input
Speed vi

Desired voltag
vi
Actual
Error Motor vi


speed e speed
vi
vi voltag and vi

transducer Amplifier
+ e drive
vi



system
-
Dancer vi

Dancer
position
Voltage sensor dynamic
vi



proportion
vi s
al
to actual speed
vi vi