Wayground logo

Free Printable Worksheets

Font size

S
M
L
XL
Worksheets

M13-4 GPS/GNSS

Total questions: 26

Worksheet time: 13mins

Name
Class
Date
1.

What type of data is contained in Block I of the GPS navigation message?

a)

Ephemeris prediction parameters

b)

Clock correction parameters

c)

Approximation of the atmospheric delay

d)

Almanac data

2.

What does AOD indicate in Block I of the GPS navigation message?

a)

Approximation of the atmospheric delay

b)

Time since the last navigation upload

c)

Clock correction parameters

d)

Ephemeris prediction parameters

3.

What type of data is contained in Block III of the GPS navigation message?

a)

Almanac data

b)

Clock correction parameters

c)

Approximation of the atmospheric delay

d)

Ephemeris prediction parameters

4.

What is the primary factor for the safety of a navigation system according to the text?

a)

Accuracy

b)

Availability

c)

Continuity

d)

Integrity

5.

What does DOP stand for in the context of GPS accuracy?

a)

Differential of Precision

b)

Dilution of Precision

c)

Direction of Position

d)

Distance of Position

6.

What is the minimum percentage of time that the GPS SPS is mandated to be available according to the 1996 Federal Radio navigation Plan?

a)

99.85%

b)

95%

c)

98%

d)

99%

7.

What does RAIM stand for in the context of GPS navigation?

a)

Remote Access and Integrity Monitoring

b)

Rapid Assessment of Integrity Monitoring

c)

Receiver Autonomous Integrity Monitoring

d)

Radio Aided Integrity Monitoring

8.

What is the primary purpose of Differential GPS?

a)

To improve measurement precision by using differential methods

b)

To provide precise positioning service for military users

c)

To enhance the availability of GPS signals

d)

To monitor the integrity of GPS satellites

9.

Why is there a need to have reception from 5 satellites to use GPS in aviation?

a)

To obtain height information as well as lateral position

b)

To detect anomalies in Space Vehicles used the navigation solution

c)

Without the fifth satellite only a poor GDOP can be achieved.

10.

What mode does the GPSSU enter when it has decoded ephemeris data to compute a navigation solution?

a)

Navigation mode

b)

Initialization mode

c)

Self-Test mode

d)

Acquisition mode

11.

What is the purpose of the 'Pseudorange' in GPS technology?

a)

To measure the distance between the GPS receiver and the satellite

b)

To determine the speed of the GPS receiver

c)

To calculate the time delay in GPS signal transmission

d)

To estimate the position of the GPS receiver

12.

What does the 'Ephemeris' data in a GPS signal provide?

a)

Information about the GPS satellite's health status

b)

Information about the GPS satellite's precise orbital location

c)

Information about the atmospheric conditions affecting the GPS signal

d)

Information about the GPS satellite's clock correction parameters

13.

What is the purpose of the 'Clock Correction Parameters' in the GPS navigation message?

a)

To correct the time delay in GPS signal transmission

b)

To correct the GPS receiver's internal clock

c)

To correct the GPS satellite's atomic clock

d)

To correct the time difference between the GPS receiver and the satellite

14.

What is the best position for satellites for good GDOP?

a)
Evenly spread out around the receiver
b)
Clustered in one area around the receiver
c)
Randomly scattered around the receiver
d)
Concentrated in a single line around the receiver
15.

What is the basic concept behind GPS?

a)

Measuring the color of satellites in space

b)

Measuring the temperature of satellites in space

c)

Measuring the speed of satellites in space

d)

Measuring the distance from a group of satellites in space

16.

How many satellite ranges are needed to unambiguously locate a position?

a)

Three

b)

Four

c)

Two

d)

One

17.

What is the purpose of the Master Control Station in Colorado Springs?

a)

To monitor the health of GPS receivers

b)

To control the orbits and clocks of GPS satellites

c)

To transmit corrections to GPS satellites

d)

To measure the altitude of GPS satellites

18.

How many GPS satellites are in orbit?

a)

24

b)

18

c)

30

d)

12

19.

What is the function of the GPS receiver in an aircraft?

a)

To generate the navigation message

b)

To convert satellite signals into position, time, and velocity

c)

To control the orbits of GPS satellites

d)

To transmit corrections to GPS satellites

20.

What is the frequency of the L1 signal transmitted by GPS satellites?

a)

50 bps

b)

10.23 MHz

c)

1227.60 MHz

d)

1575.42 MHz

21.

What type of GPS antenna design is commonly used in modern aircraft?

a)

Side mounted low profile antenna

b)

Rear mounted omnidirectional antenna

c)

Top mounted active antenna

d)

Bottom mounted passive antenna

22.

What is the frequency of the P/Y-code?

a)

1575.42 MHz

b)

1227.60 MHz

c)

10.23 MHz

d)

50 bps

23.

What type of data is included in the navigation message transmitted by GPS satellites?

a)

Status of the space vehicle

b)

Weather information

c)

Satellite images

d)

Radio frequencies

24.

What is the function of the almanac data in a GPS system?

a)

To provide information about the health of the satellite

b)

To provide information about the current date and time

c)

To provide information about the orbits of all GPS satellites

d)

To provide information about the location of the GPS receiver

25.

What is the function of the atomic clocks in GPS satellites?

Select all correct answers

a)

To provide precise timekeeping for the satellite's onboard computer

b)

To provide the time stamp for the navigation message

c)

To provide the frequency for the GPS signals

d)

To provide provide synronisation for communication from user segments

26.

Which of these statements for GPS accuracy is correct?

a)

The largest error is produced by the ionospheric delay and can be corrected by all users using the 2 frequencies transmitted from the satellite.

b)

Geometric Dilution Of Precision depends on Position, Horizontal and Vertical only.

c)

σp=GDOP x σm and the optimum position is one satellite overhead and three on the horizon, 120° apart in azimuth