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The block diagram shown in the figure describes a servomotor deployed in position control of an aileron on an aircraft wing model. 1 R(s) , → K, H K,► s(s + a) - 4 K (Hint: To answer the following questions, you will need to use block diagram reduction techniques on the above block diagram, and thereby calculate the closed- loop Output Transfer Function and the closed-loop Error Transfer Function). For K2 = 0.8, Kg = 0, a = 2.8, find the required value of the gain K1 to achieve a steady-state error of 0.1 for a unit-ramp input.

The block diagram shown in the figure describes a servomotor deployed in position control of an aileron on an aircraft wing model. 1 R(s) , → K, H K,► s(s + a) - 4 K (Hint: To answer the following questions, you will need to use block diagram reduction techniques on the above block diagram, and thereby calculate the closed- loop Output Transfer Function and the closed-loop Error Transfer Function). For K2 = 0.8, Kg = 0, a = 2.8, find the required value of the gain K1 to achieve a steady-state error of 0.1 for a unit-ramp input.

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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The block diagram shown in the figure describes a servomotor deployed in position control of an aileron on an aircraft wing model. 1 R(s) , → K, H K,► s(s + a) - 4 K (Hint: To answer the following questions, you will need to use block diagram reduction techniques on the above block diagram, and thereby calculate the closed- loop Output Transfer Function and the closed-loop Error Transfer Function). For K2 = 0.8, Kg = 0, a = 2.8, find the required value of the gain K1 to achieve a steady-state error of 0.1 for a unit-ramp input.
Transcribed Image Text:The block diagram shown in the figure describes a servomotor deployed in position control of an aileron on an aircraft wing model. 1 R(s) , → K, H K,► s(s + a) - 4 K (Hint: To answer the following questions, you will need to use block diagram reduction techniques on the above block diagram, and thereby calculate the closed- loop Output Transfer Function and the closed-loop Error Transfer Function). For K2 = 0.8, Kg = 0, a = 2.8, find the required value of the gain K1 to achieve a steady-state error of 0.1 for a unit-ramp input.
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