Friday, April 25, 2014

B.E Aeronautical Engineering, Control Systems for Aircraft, Chennai Sathyabama University, Question Paper 2013

Get an old, previous years question paper (2013 question paper) of Control Systems for Aircraft for B.E Aeronautical Engineering from the following post. It belongs to Chennai Sathyabama University. Read the question paper and make the best of it.

SATHYABAMA UNIVERSITY
(Established under section 3 of UGC Act,1956)
Course & Branch :B.E - AERO
Title of the Paper : Control Systems for Aircraft Max. Marks:80
Sub. Code : SAEX1014(2010) Time : 3 Hours
Date : 20/04/2013 Session : AN

PART - A (10 x 2 = 20)
Answer ALL the Questions

1. What is control system?

2. Define closed loop control system.

3. What is PI controller?

4. Name the test signals used in control system.

5. What are frequency domain specifications?

6. Define Bandwidth.

7. What is the necessary condition for stability?

8. What is routh stability condition?

9. Write the necessary frequency domain specification for design of a control system.

10. Why compensation is necessary in feedback control system?

Note: Part B will be in the image format below. As it involves equations, we can't able to write it fully here. Refer the images which give the complete question papers including the Part-A.

Duraimani

B.E Civil Engineer Graduated from Government College of Engineering Tirunelveli in the year 2016. She has developed this website for the welfare of students community not only for students under Anna University Chennai, but for all universities located in India. That's why her website is named as www.IndianUniversityQuestionPapers.com . If you don't find any study materials that you are looking for, you may intimate her through contact page of this website to know her so that it will be useful for providing them as early as possible. You can also share your own study materials and it can be published in this website after verification and reviewing. Thank you!