BE Avionics Engineering


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BE Avionics Engineering Quiz

1 / 25

Which is the most dominant force in spacecraft  flight dynamics;-

2 / 25

A time shared multiplex highway is used in Federated avionics architecture:-

3 / 25

FMS refers to:-

4 / 25

Which mode of Loran C requires a minimum of 3 transmitters with iterative computation  to obtain a fix:-

5 / 25

Angle of attack of the vertical tail is also known as :-

6 / 25

Which methods break the signal into finite segments to find the ASF:-

7 / 25

Which is known as the stretched A320;-

8 / 25

The information signal is otherwise referred to as:-

9 / 25

A device that can both transmit and receive is called as:-

10 / 25

Which controls the pitch of an aircraft:-

11 / 25

What happens if an aircraft yaws about its centre of  gravity:-

12 / 25

What is the full form of ARINC:-

13 / 25

The short term propagation effect caused by local weather changes are called as:-

14 / 25

Which is not one of the functions performed by the FMS:-

15 / 25

VORTAC navigation aids comprises which facilities:-

16 / 25

In omega system , a given frequency is transmitted by only one station at given time;-

17 / 25

Under which category does zero visibility conditions come:-

18 / 25

How is the velocity of an aircraft measured by passive  radio system:-

19 / 25

When a decibel value is computed by comparing a power value to 1 mW it is called as:-

20 / 25

A flight management system is not necessary for simple UAVs;-

21 / 25

Which is false with respect to MEMS gyros:-

22 / 25

What can occur when the control valve travel limits are reached under conditions of large amplitude demand:-

23 / 25

A FBW controls stick is referred as:-

24 / 25

The type of Ethernet data bus adapted for airborne application is;-

25 / 25

For a radar set with a pulse width of 25 micro seconds and a PRF of 600 pulse persecond, what is  the duty cycle:-

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