GNSS/GPS Flashcards

1
Q

Name the 3 segments in the GPS system architecture.

A

Space- satellites

Ground- ground based tracking and system adjustment

User- receiver and processor

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2
Q

State the number of satellites in a fully operational constellation with global coverage.

A

24

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3
Q

How many times per day does a satellite orbit the earth?

A

Twice

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4
Q

Who monitors the satellite constellation status and corrects for any errors?

A

Master Control Station (MCS)

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5
Q

What is Ephemeris?

A

Information transmitted by satellites about their location (current and predicted), timing and ‘health’.

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6
Q

What is the minimum number of satellites a receiver requires before it can calculate:

a. 2D position?
b. 3D position?

A

a. 3

b. 4

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7
Q

What is the name given to the type of code used in the GPS signal?

A

Pseudo random codes. (Though they are actually very well defined and predictable)

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8
Q

Name 7 errors that can degrade the accuracy of the system.

A
  1. Ephemeris
  2. Clock
  3. Receiver
  4. Atmospheric/ionosphere
  5. Multipath
  6. Masking function
  7. Selective availability
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9
Q

What is the definition of ‘integrity’ when describing the performance criteria of a navigation satellite?

A

Ability of the system to provide timely warnings to the user when the equipment is unreliable for navigation purposes.

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10
Q

What does RAIM mean?

A

Receiver Autonomous Integrity Monitoring

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11
Q

Describe the function RAIM in GPS receiver software?

A

RAIM provides integrity by detecting the failure of a GNSS satellite.

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12
Q

What is the minimum number of satellites a receiver needs before RAIM can be effective?

A

RAIM (FD) requires 5 satellites. FDE requires 6.

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13
Q

Does a large PDOP indicate the chance of a high level of accuracy or a low level of accuracy?

A

Low level of accuracy.

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14
Q

If cruising in CTA, at what period after RAIM loss must ATC be notified?

A

5 minutes

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15
Q

Can a TSO C-129 receiver be used as a sole and primary means of navigation?

A

Yes, however provision for alternate planning may not be based on RNAV approach capability.

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16
Q

When conducting a GPS arrival, what conditions must be met?

A

Primary azimuth guidance must be provided by an associated VOR or NDB.

17
Q

Is it permissible to make a GPS arrival when the destination azimuth aid is u/s?

A

No

18
Q

Masking disregards signals from satellites below the angle of?

A

TSO 129 specified a mask angle of 7.5 degrees.

19
Q

If the satellite and receiver clocks and out of synchronisation by 1/1000th of a second, the distance measurement could be in the order of?

A

More than 150NM

20
Q

The PDOP for enroute IFR navigation required is?

A

Less than 6

21
Q

What are the airworthiness requirements for GPS to be used for enroute IFR?

A
  1. TSO C129, C129A, C145A or C146A
  2. Fitted in accordance with AC21-36 and automatic barometric aiding options functional.
  3. Instructions carried on board.