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Earth Station
Subsystems
By
Ms. Madhuri N. Sachane
Earth Station
• Introduction
• The role of an Earth station
• Types of Earth station
• Earth station subsystems
• Earth station figure-of-merit
• Services offered by Earth stations
Earth Station
• The earth segment of satellite communication system
mainly consists of three earth stations.
• There are three categories of earth stations
• Transmit and receive type: The earth station can transmit
signal for satellite and receive signal from satellite.
• These stations are used for two way communication like
telephony, data transfer.
• Receive only type: These earth stations can only receive the
signal from a satellite.
• Mostly used in CATV systems.
• Transmit only type: here the earth stations can transmit
signal only towards satellite.
• Mostly used in data collection systems.
Earth Station
• Block Diagram of Earth Station
• Designing of an Earth station depends not only on the
location of earth station but also on some other factors.
• The depending factors are type of service providing, frequency
bands utilization, transmitter, receiver and antenna
characteristics.
Earth Station
• Block Diagram of Earth Station
• Digital information in the form of binary digits from terrestrial
networks enters earth station and is then processed (filtered,
multiplexed, formatted etc.) by the base band equipment.
• The encoder performs error correction coding to reduce the
error rate, by introducing extra digits into digital stream
generated by the base band equipment.
• The extra digits carry information. The presence of noise and
non-ideal nature of any communication channel produces error
rate is established above which the received information is not
stable.
• The function of the modulator is to accept the symbol stream
from the encoder and use it to modulate an intermediate
frequency (I.F) carrier.
Earth Station
• Block Diagram of Earth Station
• In satellite communication, I.F carrier frequency is chosen
at 70 MHz for communication using a 36 MHz transponder
bandwidth and at 140 MHz for a transponder bandwidth of
54 or 72 MHz.
• The I.F is needed because it is difficult to design a
modulator that works at the uplink frequency of 6 GHz (or
14GHz) directly.
• The modulated I.F carrier is fed to the up-converter and
frequency-translated to the uplink r-f frequency.
• This modulated R.F carrier is then amplified by the high
power amplifier (HPA) to a suitable level for transmission
and radiation by the antenna to the satellite.
Earth Station
• Block Diagram of Earth Station
• On the receive side, the earth station antenna receives the
low-level modulated R.F carrier in the downlink frequency
spectrum.
• The low noise amplifier (LNA) is used to amplify the weak
received signals and improve the signal to Noise ratio
(SNR). The error r ate requirements can be met more easily.
• R.F is to be reconverted to I.F at 70 or 140 MHz because it is
easier design a demodulation to work at these frequencies
than 4 or 12 GHz.
• The demodulator estimate which of the possible symbols
was transmitted based on observation of the received if
carrier.
Earth Station
• Block Diagram of Earth Station
• The decoder performs a function opposite that of the
encoder. Because the sequence of symbols recovered by the
demodulator may contain errors.
• The decoder must use the uniqueness of the redundant
digits introduced by the encoder to correct the errors and
recover information-bearing digits.
• The information stream is fed to the base-band equipment
for processing for delivery to the terrestrial network.
• The tracking equipments track the satellite and align the
beam towards it to facilitate communication.
Earth Station Subsystems
• There are four major subsystems that are present in any
earth station. Those are transmitter, receiver, antenna and
tracking subsystem.
• The ground station, or earth station, is the terrestrial base of
the system.
• The ground station communicates with the satellite to carry
out the designated mission.
• The earth station consists of major subsystems:
–The transmit subsystem
–The receive subsystem
–The antenna subsystem
–The tracking subsystem
–Power subsystem
Earth Station Subsystems
• Transmitter Subsystems
• The uplink is the transmitting subsystem of the earth station.
• It consists of all the electronic equipment that takes the signal
to be transmitted, amplifies it, and sends it to the antenna.
• In a communication system, the signals to be sent to the
satellite might be TV programs, multiple telephone calls, or
digital data from a computer.
• Signals modulate a carrier, are amplified, and sent to an
antenna via waveguides, combiners, and diplexers.
Earth Station Subsystems
• Transmit Ground Control Equipment
• The transmit subsystem begins with the baseband signals,
which are first fed to a multiplexer, if multiple signals are to be
carried by a single transponder.
• The multiplexer output is then fed to a modulator.
• In analog systems, a wideband frequency modulator is normally
used.
• In digital systems, analog signals are first digitized with PCM
converters.
• The resulting serial digital output is then used to modulate a
QPSK modulator
Earth Station Subsystems
• Receive Subsystems
• The downlink is the receive subsystem of the earth station.
• It usually consists of very low noise preamplifiers that take the
small signal received from the satellite and amplify it to a level
suitable for further processing.
• The signal is then demodulated and sent on to other parts of the
communication system.
• The receive subsystem consists of the LNA, down converters,
and related components.
• The purpose of the receive subsystem is to amplify the downlink
satellite signal and translate it to a suitable intermediate
frequency.
• The IF signal is then demodulated and de-multiplexed as
necessary to generate the original baseband signals.
Earth Station Subsystems
• Receiver Ground Control Equipment
• The receiver ground control equipment (GCE) consists of
one or more racks of equipment used for demodulating and de-
multiplexing the received signals.
• The down converters provide initial channelization by
transponder, and the demodulators and de-multiplexing
equipment process the 70-MHz IF signal into the original
baseband signals.
• Other intermediate signals may be developed as required by the
application.
Earth Station Subsystems
• Antenna subsystem
• The major parts of Earth station Antenna are feed
system and Antenna reflector.
• These two parts combined together radiates or receives
electromagnetic waves.
• Since the feed system obeys reciprocity theorem, the earth
station antennas are suitable for both transmitting and
receiving electromagnetic waves.
• Parabolic reflectors are used as the main antenna in
earth stations.
• The gain of these reflectors is high.
• They have the ability of focusing a parallel beam into a point
at the focus, where the feed system is located.
Earth Station Subsystems
• Tracking Subsystem
• The Tracking subsystem keeps track with the satellite and
make sure that the beam comes towards it in order to establish
the communication.
• The Tracking system present in the earth station performs
mainly two functions.
• Those are satellite acquisition and tracking of satellite.
• This tracking can be done in one of the following ways.
• Those are automatic tracking, manual tracking & program
tracking.
Earth Station Subsystems
• a)Satellite Acquisition
• Before communication can be established it is necessary to
acquire a satellite.
• One method is to program the antenna to perform a scan
around the predicted position of the satellite.
• The automatic tacking is switched on when the receiver signal
strength is sufficient to lock the tracking receiver to the
beacon.
• b)Automatic Tracking
• After acquisition a satellite needs to be tracked continuously.
• This function is performed by the automatic tracking system.
Auto-tack systems are closed-loop control systems and are
therefore highly accurate.
• This tracking mode is the preferred configuration when
accuracy is the dominant criterion.
Earth Station Subsystems
• c)Manual track:
• To avoid a total loss of communication due to a failure in the
tracking system, earth stations generally also have manual
mode.
• In this mode an antenna is moved through manual commands.
• d)Program Track:
• In this tracking mode the antenna is driven to the predicted
satellite position by a computer.
• The satellite position predictions are usually supplied by the
satellite operators.
• It may be noted that since a program track system is an open-
loop control system, its accuracy is mainly governed by the
accuracy of the prediction data.
Earth Station Subsystems
• Communication satellites transmit a beacon which is used
by earth stations for tracking. The received beacon signal is
fed into the auto-track receiver where tracking corrections
or, in some auto-track systems estimated positions of the
satellite are derived.
MAIN ELEMENTS OF A
SATELLITE TRACKING SYSTEM
Earth Station Subsystems
• Tracking Subsystem
• In other auto-track techniques the feed system provides the
required components of error signals.
• The outputs of the auto-track receivers are processed and used
to drive each axis of the antenna to the estimated satellite
position.
• In the manual mode, an operator sets the desired angles for
each axis on a control console.
• This position is compared with the actual antenna position
obtained through shaft encoders, and the difference signal is
used to drive the antenna.
• In the program track mode the desired antenna position is
obtained from a computer.
• The difference in the desired antenna positions constitutes the
error and is used to drive the antenna.
Earth Station Subsystems
• Telemetry and Control Subsystems
• The telemetry equipment consists of a receiver and the
recorders and indicators that display the telemetry signals.
• The signal may be received by the main antenna or a
separate telemetry antenna.
• A separate receiver on a frequency different from that of the
communication channels is used for telemetry purposes.
• The electronic equipment used to deal with the information
transmitted back to the earth station.
Earth Station Subsystems
• Power Subsystems
• Most earth stations receive their power from the normal ac
mains.
• Standard power supplies convert the ac power to the dc
voltages required to operate all subsystems.
• Most earth stations have backup power systems that take over
if an ac power failure occurs.
• The backup power system may consist of a diesel engine
driving an ac generator, which automatically starts when ac
power fails.
• Smaller systems may use uninterruptible power supplies
(UPS), which derive their main power from batteries.
Thank you

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Earth Station Subsystem

  • 2. Earth Station • Introduction • The role of an Earth station • Types of Earth station • Earth station subsystems • Earth station figure-of-merit • Services offered by Earth stations
  • 3. Earth Station • The earth segment of satellite communication system mainly consists of three earth stations. • There are three categories of earth stations • Transmit and receive type: The earth station can transmit signal for satellite and receive signal from satellite. • These stations are used for two way communication like telephony, data transfer. • Receive only type: These earth stations can only receive the signal from a satellite. • Mostly used in CATV systems. • Transmit only type: here the earth stations can transmit signal only towards satellite. • Mostly used in data collection systems.
  • 4. Earth Station • Block Diagram of Earth Station • Designing of an Earth station depends not only on the location of earth station but also on some other factors. • The depending factors are type of service providing, frequency bands utilization, transmitter, receiver and antenna characteristics.
  • 5. Earth Station • Block Diagram of Earth Station • Digital information in the form of binary digits from terrestrial networks enters earth station and is then processed (filtered, multiplexed, formatted etc.) by the base band equipment. • The encoder performs error correction coding to reduce the error rate, by introducing extra digits into digital stream generated by the base band equipment. • The extra digits carry information. The presence of noise and non-ideal nature of any communication channel produces error rate is established above which the received information is not stable. • The function of the modulator is to accept the symbol stream from the encoder and use it to modulate an intermediate frequency (I.F) carrier.
  • 6. Earth Station • Block Diagram of Earth Station • In satellite communication, I.F carrier frequency is chosen at 70 MHz for communication using a 36 MHz transponder bandwidth and at 140 MHz for a transponder bandwidth of 54 or 72 MHz. • The I.F is needed because it is difficult to design a modulator that works at the uplink frequency of 6 GHz (or 14GHz) directly. • The modulated I.F carrier is fed to the up-converter and frequency-translated to the uplink r-f frequency. • This modulated R.F carrier is then amplified by the high power amplifier (HPA) to a suitable level for transmission and radiation by the antenna to the satellite.
  • 7. Earth Station • Block Diagram of Earth Station • On the receive side, the earth station antenna receives the low-level modulated R.F carrier in the downlink frequency spectrum. • The low noise amplifier (LNA) is used to amplify the weak received signals and improve the signal to Noise ratio (SNR). The error r ate requirements can be met more easily. • R.F is to be reconverted to I.F at 70 or 140 MHz because it is easier design a demodulation to work at these frequencies than 4 or 12 GHz. • The demodulator estimate which of the possible symbols was transmitted based on observation of the received if carrier.
  • 8. Earth Station • Block Diagram of Earth Station • The decoder performs a function opposite that of the encoder. Because the sequence of symbols recovered by the demodulator may contain errors. • The decoder must use the uniqueness of the redundant digits introduced by the encoder to correct the errors and recover information-bearing digits. • The information stream is fed to the base-band equipment for processing for delivery to the terrestrial network. • The tracking equipments track the satellite and align the beam towards it to facilitate communication.
  • 9. Earth Station Subsystems • There are four major subsystems that are present in any earth station. Those are transmitter, receiver, antenna and tracking subsystem. • The ground station, or earth station, is the terrestrial base of the system. • The ground station communicates with the satellite to carry out the designated mission. • The earth station consists of major subsystems: –The transmit subsystem –The receive subsystem –The antenna subsystem –The tracking subsystem –Power subsystem
  • 10. Earth Station Subsystems • Transmitter Subsystems • The uplink is the transmitting subsystem of the earth station. • It consists of all the electronic equipment that takes the signal to be transmitted, amplifies it, and sends it to the antenna. • In a communication system, the signals to be sent to the satellite might be TV programs, multiple telephone calls, or digital data from a computer. • Signals modulate a carrier, are amplified, and sent to an antenna via waveguides, combiners, and diplexers.
  • 11. Earth Station Subsystems • Transmit Ground Control Equipment • The transmit subsystem begins with the baseband signals, which are first fed to a multiplexer, if multiple signals are to be carried by a single transponder. • The multiplexer output is then fed to a modulator. • In analog systems, a wideband frequency modulator is normally used. • In digital systems, analog signals are first digitized with PCM converters. • The resulting serial digital output is then used to modulate a QPSK modulator
  • 12. Earth Station Subsystems • Receive Subsystems • The downlink is the receive subsystem of the earth station. • It usually consists of very low noise preamplifiers that take the small signal received from the satellite and amplify it to a level suitable for further processing. • The signal is then demodulated and sent on to other parts of the communication system. • The receive subsystem consists of the LNA, down converters, and related components. • The purpose of the receive subsystem is to amplify the downlink satellite signal and translate it to a suitable intermediate frequency. • The IF signal is then demodulated and de-multiplexed as necessary to generate the original baseband signals.
  • 13. Earth Station Subsystems • Receiver Ground Control Equipment • The receiver ground control equipment (GCE) consists of one or more racks of equipment used for demodulating and de- multiplexing the received signals. • The down converters provide initial channelization by transponder, and the demodulators and de-multiplexing equipment process the 70-MHz IF signal into the original baseband signals. • Other intermediate signals may be developed as required by the application.
  • 14. Earth Station Subsystems • Antenna subsystem • The major parts of Earth station Antenna are feed system and Antenna reflector. • These two parts combined together radiates or receives electromagnetic waves. • Since the feed system obeys reciprocity theorem, the earth station antennas are suitable for both transmitting and receiving electromagnetic waves. • Parabolic reflectors are used as the main antenna in earth stations. • The gain of these reflectors is high. • They have the ability of focusing a parallel beam into a point at the focus, where the feed system is located.
  • 15. Earth Station Subsystems • Tracking Subsystem • The Tracking subsystem keeps track with the satellite and make sure that the beam comes towards it in order to establish the communication. • The Tracking system present in the earth station performs mainly two functions. • Those are satellite acquisition and tracking of satellite. • This tracking can be done in one of the following ways. • Those are automatic tracking, manual tracking & program tracking.
  • 16. Earth Station Subsystems • a)Satellite Acquisition • Before communication can be established it is necessary to acquire a satellite. • One method is to program the antenna to perform a scan around the predicted position of the satellite. • The automatic tacking is switched on when the receiver signal strength is sufficient to lock the tracking receiver to the beacon. • b)Automatic Tracking • After acquisition a satellite needs to be tracked continuously. • This function is performed by the automatic tracking system. Auto-tack systems are closed-loop control systems and are therefore highly accurate. • This tracking mode is the preferred configuration when accuracy is the dominant criterion.
  • 17. Earth Station Subsystems • c)Manual track: • To avoid a total loss of communication due to a failure in the tracking system, earth stations generally also have manual mode. • In this mode an antenna is moved through manual commands. • d)Program Track: • In this tracking mode the antenna is driven to the predicted satellite position by a computer. • The satellite position predictions are usually supplied by the satellite operators. • It may be noted that since a program track system is an open- loop control system, its accuracy is mainly governed by the accuracy of the prediction data.
  • 18. Earth Station Subsystems • Communication satellites transmit a beacon which is used by earth stations for tracking. The received beacon signal is fed into the auto-track receiver where tracking corrections or, in some auto-track systems estimated positions of the satellite are derived. MAIN ELEMENTS OF A SATELLITE TRACKING SYSTEM
  • 19. Earth Station Subsystems • Tracking Subsystem • In other auto-track techniques the feed system provides the required components of error signals. • The outputs of the auto-track receivers are processed and used to drive each axis of the antenna to the estimated satellite position. • In the manual mode, an operator sets the desired angles for each axis on a control console. • This position is compared with the actual antenna position obtained through shaft encoders, and the difference signal is used to drive the antenna. • In the program track mode the desired antenna position is obtained from a computer. • The difference in the desired antenna positions constitutes the error and is used to drive the antenna.
  • 20. Earth Station Subsystems • Telemetry and Control Subsystems • The telemetry equipment consists of a receiver and the recorders and indicators that display the telemetry signals. • The signal may be received by the main antenna or a separate telemetry antenna. • A separate receiver on a frequency different from that of the communication channels is used for telemetry purposes. • The electronic equipment used to deal with the information transmitted back to the earth station.
  • 21. Earth Station Subsystems • Power Subsystems • Most earth stations receive their power from the normal ac mains. • Standard power supplies convert the ac power to the dc voltages required to operate all subsystems. • Most earth stations have backup power systems that take over if an ac power failure occurs. • The backup power system may consist of a diesel engine driving an ac generator, which automatically starts when ac power fails. • Smaller systems may use uninterruptible power supplies (UPS), which derive their main power from batteries.