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PTU B.Tech Aerospace Engineering 5th Semester May 2019 71838 CONTROL ENGINEERING Question Papers

PTU Punjab Technical University B-Tech May 2019 Question Papers 5th Semester Aerospace Engineering

This post was last modified on 04 November 2019

PTU B.Tech Dec 2018 5th Semester Question Papers || Punjab Technical University


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Roll No. | [ | [ [ ] [ [ ] Total No. of Pages : 02
Total No. of Questions : 09
B.Tech. (Aerospace Engineering) (2012 Onwards) (Sem.-5)
CONTROL ENGINEERING
Subject Code : ASPE-304

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M.Code : 71838
Time : 3 Hrs. Max. Marks : 60

INSTRUCTIONS TO CANDIDATES :

  1. SECTION-A is COMPULSORY consisting of TEN questions carrying TWO marks each.
  2. SECTION-B contains FIVE questions carrying FIVE marks each and students have to attempt any FOUR questions.
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  4. SECTION-C contains THREE questions carrying TEN marks each and students have to attempt any TWO questions.

SECTION-A

  1. Write briefly :
    1. Block representation of system elements
    2. Bode attenuation diagram
    3. Concept of automatic control
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    5. Proportional controller
    6. Phase margin
    7. Closed loop system
    8. Modern control theory
    9. Relative stability
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    11. Mason’s Gain formula
    12. Polar plot

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SECTION-B

  1. Determine whether the characteristic equation given below has stable or unstable roots.(5)
    20 +4+40+12=0
  2. How addition of poles and zeros affect the stability characteristics of a closed loop system? (5)
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  4. Illustrate the first order system response to step, ramp and impulse input with the help of examples.
  5. Distinguish between ‘PI” and ‘PID’ controllers.
  6. Write short notes on ‘M & N Circles’.

SECTION-C

  1. What do you mean by compensation? Explain Series and Feedback compensation. Discuss the physical devices used for system compensation. 2,4,4
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  3. An airplane is found to have poor short period flying qualities in a particular flight regime. To improve the flying qualities; a stability augmentation system using state feedback is to be employed. Determine the feedback gains so that the airplane’s short period characteristics are Asp = =211 + 2.14i. Assume that the original short period dynamics are given as : (10)
    Aa] [-0334 1.0 Aol [-0.027
    . |= + [A8,]
    Ag =252 -0387||Aag | |26
  4. What do you mean by transfer function and transfer function models? Explain the transfer function models for mechanical and thermal systems with the help of examples.(4, 6)
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NOTE : Disclosure of Identity by writing Mobile No. or Making of passing request on any page of Answer Sheet will lead to UMC against the Student.


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