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Download PTU B.Tech 2020 March Aero 5th Sem ASPE 304 Control Engineering Question Paper

Download PTU (I.K. Gujral Punjab Technical University Jalandhar (IKGPTU) ) BE/BTech Aero (Aerospace-Engg) 2020 March 5th Sem ASPE 304 Control Engineering Previous Question Paper

This post was last modified on 21 March 2020

PTU B.Tech Question Papers 2020 March (All Branches)


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Roll No. [ ] Total No. of Pages : 03
Total No. of Questions : 09

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B.Tech. (Aerospace Engineering) (2012 Onwards) (Sem.-5)
CONTROL ENGINEERING
Subject Code : ASPE-304
M.Code : 71838
Time : 3 Hrs. Max. Marks : 60

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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.
  3. SECTION-C contains THREE questions carrying TEN marks each and students have to attempt any TWO questions.

SECTION-A

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  1. Write briefly :
    1. State the properties of transfer function.
    2. What is servomechanism?
    3. State Nyquist stability criterion.
    4. Name and define types of controllers.
    5. Write down Mason’s-gain formula and explain its various terms.
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    7. What is Force-voltage analog?
    8. Explain the terms phase margin and gain margin.
    9. Name the physical devices for system compensation.
    10. What is Bode plot?
    11. State Routh’s Hurwitz criterion.
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SECTION-B

  1. A system for controlling the position of a robot is shown in fig. 1. Use a proportional plus integral controller to design a system whose characteristic equation has a damping ratio g = 1.0 and a natural frequency ?n = 4. Determine K.
  2. For the mechanical system shown in Fig. 2.
    1. Determine the differential equation relating f and x.
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    3. Construct the force voltage analog.
    4. Construct the force current analog.
  3. Draw the complete signal flow graph for the following simultaneous equations :
    X1 = a11x1 + a12x2 + b1u1

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    X2 = a21x1 + a22x2 + b2u2
  4. The block diagram representation for a servomechanism is shown in fig. 3.
    Determine the differential equation relating the output y to the input x. Determine the value of the steady state gain & and the time constant t.
  5. Illustrate the use of a phase-lead component placed in series with the feedback portion of a control system to improve the stability.

SECTION-C

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  1. The open-loop transfer function of a control system is
    Determine the value of G (j?) H(j?)/K for ?=0, 1,2, 3,4, 5 and 6
    Construct the entire Nyquist plot and then determine the range of values of K such that the system is stable.
  2. The block diagram for the autopilot for a large commercial airliner is shown in fig. 4. The system is to be designed such that the percentage of overshoot to a step change in the input does not exceed 10 percent, and the 5 percent settling time should be less than 1s.
    Determine the required values of K and a.
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  4. A system for controlling the output torque from an engine is shown in fig. 5. Apply Routh’s criterion to determine the range of values of a such that the system is stable.

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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