BE Avionics Engineering

BE Avionics Engineering

13

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BE Avionics Engineering Quiz

1 / 25

A two stage amplifier has an input power of 30 μW and output power of 1.5 mW.one stage has a gain of 3. What is the gain of the second stage:-

2 / 25

What should be the gain of an amplifier to have no voltage loss or gain:-

3 / 25

A  mode  S  transponder  is  silent  when  it is  not  interrogated :-

4 / 25

Fourier  analysis  helps us  to  determine  how much bandwidth  a particular  signal occupies :-

5 / 25

The process of making the signal more compatible with the medium is called as:-

6 / 25

Which frequency  band  is  used for   connecting   the satellite   system  with the  public  switched   telephone  network :-

7 / 25

In SDF floated gyros three gimbals are used:-

8 / 25

What is  connected between the antenna  and  the mixer  to avoid  oscillator   radiation;-

9 / 25

What type of cable does MIL  STD 1553 use;-

10 / 25

In what type of display is the image projected directly to the retina of the pilot :-

11 / 25

Earth be considered as a communication medium:-

12 / 25

A highly  stable  aircraft  is  not  easily  maneuverable :-

13 / 25

Which aircraft requires the longest runway  for take off:-

14 / 25

what is the  total  power  if the carrier  power is  30 w  and the  %age  of  modulation is 85 %:-

15 / 25

What is  the main weakness of  the ILS  system ;-

16 / 25

When is the speed  of the satellite  maximum  in   an elliptical  orbit :-

17 / 25

Air  traffic  control  and   traffic  flow  management  are  two principal  processes  of  air  ttrafic  management :-

18 / 25

When does  an ILS   coupling  loop  become  unstable :-

19 / 25

Which is not true about integrated modular avionics architecture:-

20 / 25

What control does  the EFIS  control panel  provide :-

21 / 25

what is the process  of  digital communication where  a  threshold  value is set  at the  receiver to reduce noise :-

22 / 25

The instantaneous FOV changes with the position view:-

23 / 25

Which is a data transfer standard for aircraft avionics:-

24 / 25

The response of a jet engine  thrust to the throttle angle is instantaneous:-

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________ Is exponential  path tangent  to  a  horizontal plane  several  feet  below  the  runway :-

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