Vayudoot Aviation

1. The orbital height and inclination of the NAVSTAR/GPS constellation are

19099 km, 55°

20180 km, 65°

19099 km, 65°

20180 km, 55°

2. The navigation and system data message is transmitted through the

50 Hz modulation

The P code

The C/A code

The C/A and P PRN codes

3. The purpose of the pseudo-random noise codes in NAVSTAR/GPS is to

pass the navigation and system data

pass the almanac data

pass the ephemeris and time information

identify the satellites

4. The use of LAAS and WAAS remove the errors caused by

GDOP, selective availability and propagation

propagation, selective availability, satellite ephemeris and clock

elective availability, satellite ephemeris and clock

receiver clock, GDOP, satellite ephemeris and clock

5. The NAVSTAR/ GPS control segment comprises

a ground segment and the INMARSAT geostationary satellites

the space segment, the user segment and the ground segment

a master control station, a back-up control station, five monitoring stations and the INMARSAT geostationary satellites

a master control station, a back-up control station and five monitoring stations

6. The availability of two frequencies in GNSS

removes receiver clock errors

reduces propagation errors

removes SV ephemeris and clock errors

reduces errors caused by GDOP

7. An all in view receiver

checks all the satellites in view and selects the 4 with the best geometry for fixing

requires 5 satellites to produce a 4D fix

informs the operator that all the satellites required for fixing and RAIM are in available

uses all the satellites in view for fixing

8. The most accurate fixing information will be obtained from

one satellite directly overhead and 3 equally spaced at 60° above the horizon

one satellite close to the horizon and 3 equally at 60° above the horizon

four satellites spaced 90° apart at 30° above the visual horizon

one satellite directly overhead and 3 spaced 120° apart close to the horizon

9. The frequency available to non-authorised users of NAVSTAR/GPS is

1246 MHz

1227.6 MHz

1575.42 MHz

1602 MHz

10. NAVSTAR/GPS operates in the band the receiver determines position by

SHF, range position lines

UHF, range position lines

SHF, secondary radar principles

UHF, secondary radar principles

11. A LAAS requires

an accurately surveyed site on the aerodrome and a link through the INMARSAT geostationary satellites to pass corrections to X, Y & Z co-ordinates to aircraft

an accurately surveyed site on the aerodrome and a system known as a pseudolite to pass satellite range corrections to aircraft

an accurately surveyed site on the aerodrome and system known as a pseudolite to pass corrections to X, Y & Z co-ordinates to aircraft

an accurately surveyed site on the aerodrome and a link through the INMARSAT geostationary satellites to pass satellite range corrections to aircraft

12. The PRN codes are used to

determine the range of the satellites from the receiver

synchronise the receiver clocks with the satellites clocks

determine the time interval between the satellite transmission and receipt of the signal at the receiver

pass ephemeris and clock data to the receivers

13. The NAVSTAR/GPS reference system is

A geo-centred 3D Cartesian co-ordinate system fixed with reference to the sun

A geo-centred 3D Cartesian co-ordinate system fixed with reference to the prime meridian, equator and pole

A geo-centred 3D system based on latitude, longitude and altitude

A geo-centred 3D Cartesian co-ordinate system fixed with reference to space

14. The model of the earth used for NAVSTAR/GPS is

PZ84

WGS90

PZ90

WGS84

15. If a receiver has to download the almanac, the time to do this will be

2.5 minutes

12.5 minutes

15 minutes

25 minutes

16. EGNOS is

a LAAS

a system to remove errors caused by the difference between the model of the earth and the actual shape of the earth

the proposed European satellite navigation system

a WAAS

17. When using GNSS to carry out a non-precision approach the MDA will be determined using

GPS altitude

barometric altitude

Radio altimeter height

Either barometric or radio altimeter altitude

18. The initial range calculation at the receiver is known as a pseudo-range, because it is not yet corrected for

receiver and satellite clock errors and ephemeris errors

receiver and satellite clock errors

receiver and satellite clock errors and propagation errors

receiver clock errors

19. The NAVSTAR/GPS operational constellation comprises how many satellites

12

24

21

30

20. The minimum number of satellites required for receiver autonomous integrity monitoring is

4

6

3

5

21. If an aircraft manoeuvre puts a satellite being used for fixing into the wing shadow then

the receiver will maintain lock using signals reflected from other parts of the aircraft with a small degrading of positional accuracy

the receiver will automatically select another satellite with no degradation in positional accuracy

the accuracy will be unaffected

the accuracy will be temporarily downgraded

22. The minimum number of satellites required for a 3D fix is

3

6

5

4

23. Which of the following statements concerning NAVSTAR/GPS time is correct?

the satellite runs its own time based on seconds and weeks which is independent of UTC the satellite runs its own time based on seconds and weeks which is independent of UTC

satellite time is the same as UTC

satellite time is based on sidereal time

the satellite runs its own time based on seconds and weeks which is correlated with UTC

24. The position derived from NAVSTAR/GPS satellites may be subject to the following errors

ephemeris, GDOP, siting

selective availability, skywave interference, GDOP

GDOP, static interference, instrument

propagation, selective availability, ephemeris

25. The most significant error of GNSS is

Ionospheric propagation

GDOP

Receiver clock

Ephemeris

26. The most accurate satellite fixing information will be obtained from

TRANSIT & NAVSTAR/GPS

NAVSTAR/GPS & GLONASS

NAVSTAR/GPS & COSPAS/SARSAT

COSPAS/SARSAT & GLONASS

Question Bank

Questions for GNSS