Solution Manual for Control Systems Engineering, 8th Edition by Norman S. Nise ISBN: 9781119721406 | Complete Solution Guide.,

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Introduction
ANSWERSTOREVIEWQUESTIONS i.z i.z i.z




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




tothe input response (the desired output), and then correcting the output response.
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5. Under the condition that the feedback element is other than unity
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6. Actuating signal i.z




7. Multiple subsystems can time share the controller. Any adjustments to the controller can
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i.z beimplemented with simply software changes.
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8. Stability, transient response, and steady-state error i.z i.z i.z i.z i.z




9. Steady-state, transient i.z




10. It follows a growing transient response until the steady-state response is no longer visible.
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i.z Thesystem will either destroy itself, reach an equilibrium state because of saturation in driving
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i.z amplifiers, or hit limit stops. i.z i.z i.z i.z




11. Natural response i.z




12. Determine the transient response performance of the system. i.z i.z i.z i.z i.z i.z i.z




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




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




16. Transfer function - the Laplace transform of the differential equation i.z i.z i.z i.z i.z i.z i.z i.z i.z




State-space - representation of an nth order differential equation as n simultaneous first-
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orderdifferential equations
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Differential equation - Modeling a system with its differential equationi.z i.z i.z i.z i.z i.z i.z i.z i.z




SOLUTIONSTOPROBLEMS i.z i.z




50 volts i.z



1. Five turns yields 50 v. Therefore K = = 1.59
5 x 2 
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Inc.
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