The block diagram shown in the figure describes a servomotor deployed in position control of an aileron on an aircraft wing model. R(s) + 1 → K, s (s + a) 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- oop Output Transfer Function and the closed-loop Error Transfer Function). The inner feedback loop is now activated (i.e. Kg takes on a non-zero value). For K2 = 4.3, K, = 1.1, a= 2.3, find the required value of the gain Kị to achieve a damping ratio of 0.6.

The block diagram shown in the figure describes a servomotor deployed in position control of an aileron on an aircraft wing model. R(s) + 1 → K, s (s + a) 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- oop Output Transfer Function and the closed-loop Error Transfer Function). The inner feedback loop is now activated (i.e. Kg takes on a non-zero value). For K2 = 4.3, K, = 1.1, a= 2.3, find the required value of the gain Kị to achieve a damping ratio of 0.6.

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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