Q6. An electro-hydraulic actuator is used to position an aircraft control surface. The torque applied to the actuator, T, is controlled by a unity feedback control system as indicated in Figure Q.6. The resultant angular velocity of the surface is denoted by o, whilst the reference value is m. The transfer function of the controller is G(s). (a) Assuming a proportional gain controller is used, what value of gain K, will yield a steady-state error response of 1% to a unit step input? (b) To eliminate the steady-state error, an integral controller of gain K, is used. Determine the value of K; which will give an overall system damping of 0.707*- (c) A PID controller is then applied with the integral gain K, = 10. If the design specification is for a closed-loop damping factor of 0.7, calculate the necessary values of proportional and derivative gain if the system rise time to a unit step input is 0.5 seconds.

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...
icon
Related questions
Question
Q6.
An electro-hydraulic actuator is used to position an aircraft control surface.
The
torque applied to the actuator, T, is controlled by a unity feedback control system as
indicated in Figure Q.6. The resultant angular velocity of the surface is denoted by a
whilst the reference value is m The transfer function of the controller is G(s).
(a) Assuming a proportional gain controller is used, what value of gain Kp will yield
a steady-state error response of 1% to a unit step input?
(b) To eliminate the steady-state error, an integral controller of gain K, is used.
Determine the value of K, which will give an overall system damping of 0.707-
(c) A PID controller is then applied with the integral gain K, = 10. If the design
specification is for a closed-loop damping factor of 0.7, calculate the necessary
values of proportional and derivative gain if the system rise time to a unit step
input is 0.5 seconds.
(d) Calculate the maximum overshoot and settling time for this system for the
situation given in part c).
E(s)
T(s)
m(s)
1
G(s)
s+2
Figure Q6
Transcribed Image Text:Q6. An electro-hydraulic actuator is used to position an aircraft control surface. The torque applied to the actuator, T, is controlled by a unity feedback control system as indicated in Figure Q.6. The resultant angular velocity of the surface is denoted by a whilst the reference value is m The transfer function of the controller is G(s). (a) Assuming a proportional gain controller is used, what value of gain Kp will yield a steady-state error response of 1% to a unit step input? (b) To eliminate the steady-state error, an integral controller of gain K, is used. Determine the value of K, which will give an overall system damping of 0.707- (c) A PID controller is then applied with the integral gain K, = 10. If the design specification is for a closed-loop damping factor of 0.7, calculate the necessary values of proportional and derivative gain if the system rise time to a unit step input is 0.5 seconds. (d) Calculate the maximum overshoot and settling time for this system for the situation given in part c). E(s) T(s) m(s) 1 G(s) s+2 Figure Q6
Expert Solution
trending now

Trending now

This is a popular solution!

steps

Step by step

Solved in 4 steps with 4 images

Blurred answer
Knowledge Booster
Mathematical Modeling of Mechanical System
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, electrical-engineering and related others by exploring similar questions and additional content below.
Similar questions
  • SEE MORE QUESTIONS
Recommended textbooks for you
Introductory Circuit Analysis (13th Edition)
Introductory Circuit Analysis (13th Edition)
Electrical Engineering
ISBN:
9780133923605
Author:
Robert L. Boylestad
Publisher:
PEARSON
Delmar's Standard Textbook Of Electricity
Delmar's Standard Textbook Of Electricity
Electrical Engineering
ISBN:
9781337900348
Author:
Stephen L. Herman
Publisher:
Cengage Learning
Programmable Logic Controllers
Programmable Logic Controllers
Electrical Engineering
ISBN:
9780073373843
Author:
Frank D. Petruzella
Publisher:
McGraw-Hill Education
Fundamentals of Electric Circuits
Fundamentals of Electric Circuits
Electrical Engineering
ISBN:
9780078028229
Author:
Charles K Alexander, Matthew Sadiku
Publisher:
McGraw-Hill Education
Electric Circuits. (11th Edition)
Electric Circuits. (11th Edition)
Electrical Engineering
ISBN:
9780134746968
Author:
James W. Nilsson, Susan Riedel
Publisher:
PEARSON
Engineering Electromagnetics
Engineering Electromagnetics
Electrical Engineering
ISBN:
9780078028151
Author:
Hayt, William H. (william Hart), Jr, BUCK, John A.
Publisher:
Mcgraw-hill Education,