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where zeta = 0.707 and wn = 15. The transfer function of the power amplifier is approximately G₁(s) = ka TS + 1 where tau = 0.15 s. (a) Determine the sensitivity of the system to a change of the parameter ka. (b) The system is subjected to a disturbance Td(s) = 10/s. Determine the required magnitude of ka in order to maintain the steady-state error of the system less than 0.10° when the input R(s) is zero. (c) Determine the steady state error of the system when subjected to a disturbance Td(s) = 10/s when it is operating as an open-loop system ks = 0 with R(s) = 0.

where zeta = 0.707 and wn = 15. The transfer function of the power amplifier is approximately G₁(s) = ka TS + 1 where tau = 0.15 s. (a) Determine the sensitivity of the system to a change of the parameter ka. (b) The system is subjected to a disturbance Td(s) = 10/s. Determine the required magnitude of ka in order to maintain the steady-state error of the system less than 0.10° when the input R(s) is zero. (c) Determine the steady state error of the system when subjected to a disturbance Td(s) = 10/s when it is operating as an open-loop system ks = 0 with R(s) = 0.

Introductory Circuit Analysis (13th Edition)
Introductory Circuit Analysis (13th Edition)
13th Edition
ISBN:9780133923605
Author:Robert L. Boylestad
Publisher:Robert L. Boylestad
Chapter1: Introduction
Section: Chapter Questions
Problem 1P: Visit your local library (at school or home) and describe the extent to which it provides literature...
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Hi, please solve the following problem showing all steps in detail. I am reviewing this for an upcoming exam, and I want to make sure I have everything down correctly.
where zeta = 0.707 and wn = 15. The transfer function of the power amplifier is approximately G₁(s) = ka TS + 1 where tau = 0.15 s. (a) Determine the sensitivity of the system to a change of the parameter ka. (b) The system is subjected to a disturbance Td(s) = 10/s. Determine the required magnitude of ka in order to maintain the steady-state error of the system less than 0.10° when the input R(s) is zero. (c) Determine the steady state error of the system when subjected to a disturbance Td(s) = 10/s when it is operating as an open-loop system ks = 0 with R(s) = 0.
Transcribed Image Text:where zeta = 0.707 and wn = 15. The transfer function of the power amplifier is approximately G₁(s) = ka TS + 1 where tau = 0.15 s. (a) Determine the sensitivity of the system to a change of the parameter ka. (b) The system is subjected to a disturbance Td(s) = 10/s. Determine the required magnitude of ka in order to maintain the steady-state error of the system less than 0.10° when the input R(s) is zero. (c) Determine the steady state error of the system when subjected to a disturbance Td(s) = 10/s when it is operating as an open-loop system ks = 0 with R(s) = 0.
Large microwave antennas have become increasingly important for radio astronomy and satellite tracking. A large antenna with a diameter of 60 ft, for example, is susceptible to large wind gust torques. A proposed antenna is required to have an error of less than 0.10° in a 35 mph wind. Experiments show that this wind force exerts a maximum disturbance at the antenna of 200,000 ft lb at 35 mph, or the equivalent to 10 volts at the input Td(s) to the amplidyne. One problem of driving large antennas is the form of the system transfer function that possesses a structural resonance. The antenna servosystem is shown in the figure below. The transfer function of the antenna, drive motor, and amplidyne is approximated by R(s) where G(s) = Power amplifier G₁(s) T/(s) Sensor k,= 1 Antenna, drive motor, and amplidyne G(s) w/1 s(s² + 25w,s + w²/1) 0(s) Position (radians) where zeta = 0.707 and wn = 15. The transfer function of the power amplifier is approximately
Transcribed Image Text:Large microwave antennas have become increasingly important for radio astronomy and satellite tracking. A large antenna with a diameter of 60 ft, for example, is susceptible to large wind gust torques. A proposed antenna is required to have an error of less than 0.10° in a 35 mph wind. Experiments show that this wind force exerts a maximum disturbance at the antenna of 200,000 ft lb at 35 mph, or the equivalent to 10 volts at the input Td(s) to the amplidyne. One problem of driving large antennas is the form of the system transfer function that possesses a structural resonance. The antenna servosystem is shown in the figure below. The transfer function of the antenna, drive motor, and amplidyne is approximated by R(s) where G(s) = Power amplifier G₁(s) T/(s) Sensor k,= 1 Antenna, drive motor, and amplidyne G(s) w/1 s(s² + 25w,s + w²/1) 0(s) Position (radians) where zeta = 0.707 and wn = 15. The transfer function of the power amplifier is approximately
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