Radio Navigation Aids Flashcards

1
Q

VHF Omni Range (VOR)

A

Uses the concept of phase differential
Transmits a 30 Hz reference and a 30 Hz variable-phase signal
Receiver compared these and finds the radial from the station

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2
Q

VOR Errors

A

Airborne Equipment (receiver error +/- 2)
Vertical Polarisation (antenna is banked out of the horizontal plane)
Ground Station (transmission equipment +/- 2)
Aggregate (total of all errors +/- 5)
Site/terrain effect (bending or scalloping of signals due obstacles close to the site +/- 2)

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3
Q

Magnetic Variation Application VOR

A

Applied at the transmitter (calibrated)

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4
Q

Doppler VOR

A

Almost eliminated site effect by using FM

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5
Q

NDB/ADF

A

Uses ground waves
NDB radiates a non-directional signal in MF band (<200nm)
2 antennae, 1 loop giving the null position and 1 sense solving the 180 degree ambiguity

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6
Q

Locators

A

NDB with less power

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7
Q

Errors NDB/ADF

A

Mountain effect (reflected signals from mountains/hills)
Interference (co-channel, from other NBB’s which increases at night)
Night effect (sky wave interference)
Terrain effect (signals attenuated over non conductive surfaces)
Costal refraction (bent towards land as they cross the coast)
Height effect (decreased range at decreased altitude over non conductive surfaces)
Aircraft (signal bending due aircraft interference)
Thunderstorms

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8
Q

DME

A

UHF
Automatically tuned to VOR frequency
Ground transponder and aircraft transmit pulses to compute a distance
Uses actual distance (slant range) to station

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9
Q

Ground Speed DME Error

A

Ground speed readout will decrease at a;increasing rate when overflying an aid due to slant range error increasing
Will reach 0 as the aircraft passes directly overhead the aid
If not flying directly to station, ground speed will be erroneously decreasing and time to station increasing.

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10
Q

Limitations of DME

A

Line of sight only
Will only respond to the strongest signals when lots of traffic which decreases the range

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11
Q

SSR (Secondary Surveillance Error]

A

Ground based interrogator transmits requesting all transponders to respond
Can show altitude as well as range and azimuth
~110nm range

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12
Q

ILS

A

Localiser in the same band as VOR
Consists of two transmitters, 1 at 90 Hz and 1 at 150 Hz
Transmitters aligned for equal strength on the wry extended centreline

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13
Q

3 Components of the ILS

A

Localiser
Glideslope
Marker Beacons

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14
Q

ILS Full Scale Deflection of CDI

A

2.5 degrees off centreline

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15
Q

Localiser Range

A

25nm within +/- 10 degrees of the CDI + 2000ft

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16
Q

Localiser False Indications

A

Outside sector 35 degrees either side of the localiser

17
Q

Glideslope

A

Provides a 3 degree slope to the 1000ft markers
Pass threshold at 50ft

18
Q

Glideslope Full Scale Deflection

A

0.7 degrees above or below