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 :
- SECTION-A is COMPULSORY consisting of TEN questions carrying TWO marks each.
- SECTION-B contains FIVE questions carrying FIVE marks each and students have to attempt any FOUR questions.
- SECTION-C contains THREE questions carrying TEN marks each and students have to attempt any TWO questions.
SECTION-A
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- Write briefly :
- State the properties of transfer function.
- What is servomechanism?
- State Nyquist stability criterion.
- Name and define types of controllers.
- Write down Mason’s-gain formula and explain its various terms.
- What is Force-voltage analog?
- Explain the terms phase margin and gain margin.
- Name the physical devices for system compensation.
- What is Bode plot?
- State Routh’s Hurwitz criterion.
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SECTION-B
- 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.
- For the mechanical system shown in Fig. 2.
- Determine the differential equation relating f and x.
- Construct the force voltage analog.
- Construct the force current analog.
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- Draw the complete signal flow graph for the following simultaneous equations :
X1 = a11x1 + a12x2 + b1u1--- Content provided by FirstRanker.com ---
X2 = a21x1 + a22x2 + b2u2 - 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. - 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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- 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. - 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. - 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.
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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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This download link is referred from the post: PTU B.Tech Question Papers 2020 March (All Branches)