avionics and aircraft systems chapter 2 aircraft communication systems

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Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

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Page 1: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Avionics and Aircraft

Systems

Chapter 2 Aircraft Communication Systems

Page 2: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Radios used on present day aircraft are various and use different frequencies depending on the range they have to transmit to.

BAND Frequency

Wavelength

Propagation Via

Range

MF MediumFrequency

300-3,000kHz

1,000 -100m

Line of sightup to 100

miles

HF High Frequency

3-30MHz 100-10m Ionospheric Refraction

World wide depending on propagation

VHF Very High Frequency

30-300MHz

10-1m Rarely Ionospheric Refraction

Line of sight 200-250

miles

UHF Ultra High Frequency

300-3,000MH

z

100-10cm Line of sight 100-150

miles

Communication Systems

Page 3: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Allocation Of Frequencies

UHF – Mainly military use for voice communication.

VHF – Used by civilian and military for voice communicationand Data Link. Also used by navigation aids (VOR,TACAN).

HF – Used by civilian and military for voice communicationand Data Link.

MF – Used by civilian and military for navigation aids (ADF) and for civilian radio stations.

The range of these signals can vary due to the output power of the transmitters.

Communication Systems

Page 4: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Therefore by positioning a satellite in space over a specific areait can be used to extend the range of the VHF and UHF signals.

Communication Systems

VHF and UHF radio signals are line of sight and are not affected by the Ionosphere and pass directly through it.

VHFandUHF

There are two types of satellite relay:

Non-productive – Simple relay of original message.

Productive – Where the message is boosted.

Page 5: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

HF range can be badly affected by weather and ionosphere effects.

On a good day you will be able to talk to the other side of the world, but on a bad day you may be lucky to reach 100 miles.

Communication Systems

HF uses the Ionosphere to bounce it’s signals off it and so extend the range.

HF

This means it can be badly affected by weather.

This is known as radio wave propagation.

Page 6: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

A power supply circuit to transform the input electrical power to the higher voltages needed to produce the required power output.

Communication Systems Transmitters

Components.

An electronic oscillator circuit to generate the radio frequency signal. This usually generates a sine wave of constant amplitude often called the carrier wave, because it serves to "carry" the information through space.

A modulator circuit to add the information to be transmitted to the carrier wave produced by the oscillator. This is done by varying some aspect of the carrier wave.

An RF power amplifier to increase the power of the signal, to increase the range of the radio waves.

Page 7: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Communication Systems Transmitters

An impedance matching (antenna tuner) circuit to match the impedance of the transmitter to the impedance of the antenna (or the transmission line to the antenna), to transfer power efficiently to the antenna.

Components.

Power Supply

OscillatorCircuit

Modulator Amplifier Antenna

Page 8: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Communication Systems Transmitters - How They Work.

This modulation might be as simple as turning the energy on and off, or altering more subtle properties such as amplitude, frequency, phase, or combinations of these properties.

Information is provided to the transmitter in the form of an electronic signal (electrical energy), producing alternating current of a desired frequency of oscillation.The transmitter contains a system to modulate (change) some property of the energy produced to impress a signal on it.

Amplitude Modulation (AM):

This varies the strength of the transmitted carrier wave signal in proportion to the information being sent.

Frequency Modulation(FM): 

This varies the frequency of the carrier wave signal.

Page 9: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Communication Systems

This signal may need amplification before the transmitter sends the modulated electrical energy to a tuned resonant antenna.

The transmitter combines the information signal to be carried with the radio frequency signal which generates the radio waves, which is often called the carrier.

Antenna (aerial)This structure converts the rapidly changing alternating current into an electromagnetic wave(energy) that can move through free space.These antenna can be of various shape and size to achieve the required range, direction and power.

There are two main types.

Omnidirectional

Directional

Transmitters - How They Work.

Page 10: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Communication Systems AntennaOmnidirectional or only weakly directional antennas which receive or radiate more or less in all directions.

Page 11: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

AntennaCommunication Systems

Directional antennas which are intended to preferentially radiate or receive in a particular direction or directional pattern.

HF AntennaRadioAntenna

SATCOMAntenna

Page 12: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Communication Systems Antenna (aerial)

HF AerialsVHF Upper

Aircraft antenna are designed to give as little drag as possible.

Page 13: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Communication Systems Antenna (aerial)

No 2 UHF

IFF/SSR

No 2 TACAN

UHF-DF

No 2 ADF Loop No.1 HF

MATADOR(IF FITTED)

No.1 TACAN (BEACON)No.2 TACAN

No.1 and No.2

GLIDESCOPE

EGI

No 1 TACAN

No 1 ADF Loop

HF3(POST-SRIM 4085)

No.2 HF

ADF SENSE

No.2 VHF

MARKER

No.1 VHF

WEATHER RADAR

IFF/SSR

No.1 UHF

RADAR ALTIMETER

VHF NAV(VOR/LOC)

Depending on the equipment fitted to the aircraft, it may require many antenna.

Page 14: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Tuned Radio Frequency (TRF) ReceiverCommunication Systems

The electromagnetic wave is intercepted by a tuned receiving antenna. This structure captures some of the energy of the wave and returns it to the form of oscillating electrical currents.

At the receiver, these currents are demodulated, which is conversion to a usable signal form by a detector sub-system.

The receiver is "tuned" to respond preferentially to the desired signals, and reject undesired signals.

Antenna

RFAmplifie

r

RF = Radio Frequency.

DetectorAudioAmplifier

AudioOutput

Page 15: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

The principle of operation of the superheterodyne receiver depends on the use of heterodyning or frequency mixing.

Superheterodyne ReceiverCommunication Systems

The signal from the antenna is filtered sufficiently at least to reject the image frequency  and amplified.

A local oscillator in the receiver produces a sine wave which mixes with that signal, shifting it to a specific intermediate frequency (IF), usually a lower frequency.

The IF signal is itself filtered and amplified and possibly processed in additional ways.

The demodulator uses the IF signal rather than the original radio frequency to recreate a copy of the original information (such as audio).

Page 16: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Antenna

RFFilter

RFAMP

Mixer

LocalOscillato

r

IFFilte

r

AMDetector

AudioOutput

IFAMP

RF = Radio Frequency. IF = Intermediate Frequency.

Superheterodyne Receiver - AMCommunication Systems

Page 17: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Superheterodyne Receiver - FMCommunication Systems

Antenna

RFFilter

RFAMP

Mixer

LocalOscillato

r

IFFilte

r

IFAMP

PhaseDetect

or

Low PassFilter

Voltage ControlledOscillator Audio

Output

Page 18: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Data LinkCommunication Systems

Is a system where information is collated and put in a digital form and then transmitted in a short burst transmission.

The information can come from various sources.

The aircraft Flight Management Computer.

Weather broadcasts.

Aircraft systems monitoring devices.

Airborne radar pictures.

Messaging service.

There are three types of Data Link System:

Simplex

Half-Duplex

Duplex

Communication in one direction Only.

Communication in both directions but not simultaneously.

Communication in both directions simultaneously.

Page 19: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

In civil aviation, a data-link system (known as Controller Pilot Data Link Communications) is used to send information between aircraft and air traffic controllers. 

Data LinkCommunication Systems

This is to overcome the problems with short range V/UHF radios and poor HF which can make voice communication impossible.

Such systems are used for aircraft crossing the Atlantic and Pacific oceans.

This system uses the aircraft's flight management computer to send location, speed and altitude information about the aircraft to the ATC.

ATC can then send messages to the aircraft regarding any necessary changes.

Page 20: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Communication Systems

The system can also be used as a company management tool.

Data about the operation of the aircraft can be transmitted automatically to the company ground station to be analysed.

A British Airways aircraft crossing the Atlantic received a message from it’s HQ, telling the crew to shut down No 2 engine.

The ground engineers had analysed the data from the aircraft and worked out that the engine would fail imminently.

Data Link

Page 21: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Data LinkCommunication Systems

In military aviation, a data-link may also carry weapons targeting information.

The Data Link messages can be encrypted to achievesecurity.

The E3D uses it to pass it’s radar picture to command HQand to other aircraft, allowing planning and allocation of targets to be more efficient.

Page 22: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Communication Systems

Emergency Locator Transmitter (ELT)

This is a small radio which is carried in most crew lifejacketsand aircraft dinghies.

It transmits either on 243.0 MHz(Military) and 121.5 MHz(Civil).

It must be positioned upright to allow the antenna to transmitthe correct cone signal.

When an aircraft is searching for survivors it flies a specific pattern to give best chance of finding them.

When it receives the signal from the ELT it continues the pattern until it enters the Cone Of Silence.

This indicates that the aircraft is directly over the survivors.

Page 23: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Communication Systems

Emergency Locator Transmitter (ELT)

If the transmitter is pointed at the search aircraft, the aircraft will be permanently in the cone of silence and never find the survivors.

Once started the transmitter must be left on continuously to ensure that the signal is available to the search aircraft.

The transmitter signal can be received at a distance outside the visual range of the survivors and therefore they may not be able to see the aircraft.

The transmitter can be automatically initiated by:

Inflation of the lifejacket.

An inertial switch on an aircraft.

Water pressure. i.e. sinking.

Page 24: Avionics and Aircraft Systems Chapter 2 Aircraft Communication Systems

Communication Systems

Emergency Locator Transmitter (ELT)

Cone OfSilence

Modern ELTs also have a speech facility, but this drains the battery quickly.