Fundamentals of Microwave &
Satellite Technologies
Historical Perspective
 Founded during WWII
 Used for long-haul telecommunications
 Displaced by fiber optic networks
 Still viable for right-of-way bypass and
geographic obstruction avoidance
Microwave Spectrum
 Range is approximately 1 GHz
to 40 GHz
 Total of all usable frequencies under
1 GHz gives a reference on the
capacity of in the microwave range
Microwave Impairments
 Equipment, antenna, and waveguide
failures
 Fading and distortion from multipath
reflections
 Absorption from rain, fog, and other
atmospheric conditions
 Interference from other frequencies
Microwave Engineering
Considerations
 Free space & atmospheric attenuation
 Reflections
 Diffractions
 Rain attenuation
Microwave Engineering
Considerations-cont’d
 Skin affect
 Line of Sight (LOS)
 Fading
 Range
 Interference
Free Space & Atmospheric
Attenuation
 Free space & atmospheric attenuation is
defined by the loss the signal undergoes
traveling through the atmosphere.
Changes in air density and absorption by
atmospheric particles.
Reflections
 Reflections can occur as the microwave
signal traverses a body of water or fog
bank; cause multipath conditions
Diffraction
 Diffraction is the result of variations in
the terrain the signal crosses
Rain Attenuation
 Raindrop absorption or scattering of the
microwave signal can cause signal loss
in transmissions.
Skin Affect
 Skin Affect is the concept that high
frequency energy travels only on the
outside skin of a conductor and does
not penetrate into it any great distance.
Skin Affect determines the properties of
microwave signals.
Line of Sight
Fresnel Zone Clearance
 Fresnel Zone Clearance is the minimum
clearance over obstacles that the signal
needs to be sent over. Reflection or
path bending will occur if the clearance
is not sufficient.
LOS & FZC-cont’d
Fresnel Zone
D1
D2
72.2
D1 X D2
F x D
secret formula
Microwave Fading
Normal Signal
Reflective Path
Caused by multi-path reflections and heavy rains
Range
 The distance a signal travels and its
increase in frequency are inversely
proportional
 Repeaters extend range
 Back-to-back antennas
 reflectors
Range-cont’d
 High frequencies are repeated/received
at or below one mile
 Lower frequencies can travel up to 100
miles but 25-30 miles is the typical
placement for repeaters
Interference
 Adjacent Channel Interference
 digital not greatly affected
 Overreach
 caused by signal feeding past a repeater to
the receiving antenna at the next station in
the route. Eliminated by zigzag path
alignment or alternate frequency use
between adjacent stations
Components of a Microwave
System
 Digital Modem
 Radio Frequency (RF) Unit
 Antenna
Digital Modem
 The digital modem modulates the
information signal (intermediate
frequency or IF).
RF Unit
 IF is fed to the RF unit which is
mounted as close physically to the
antenna as possible (direct connect is
optimal).
Antenna
 The antenna is a passive device that
radiates the modulated signal. It is fed
by direct connect of the RF unit, coaxial
cable, or waveguides at higher
frequencies.
Waveguides
Waveguides are hollow channels of
low-loss material used to direct the
signal from the RF unit to the
antenna.
Modulation Methods
 Primarily modulated today with digital
FM or AM signals
 Digital signal remains quiet until failure
threshold bit error rate renders it unusable
Bit Error Rate (BER)
 The BER is a performance measure of
microwave signaling throughput
 10 or one error per million transmitted bits
of information
 Data fail over is at 10 ; voice traffic can
withstand this error rate
-6
-3
Diversity
 Space Diversity
 Frequency Diversity
 Hot Standby
 PRI
Space Diversity
Normal Signal
Faded Signal
Transmitter Receiver
Space Diversity-cont’d
 Space Diversity protects against multi-
path fading by automatic switch over to
another antenna place below the
primary antenna. This is done at the
BER failure point or signal strength
attenuation point to the secondary
antenna that is receiving the transmitted
signal at a stronger power rating.
Frequency Diversity
Receiver
Active XTMR
Frequency #1
Protect XTMR
Frequency #2
RCVR
Frequency #1
RCVR
Frequency #2
Transmitter
Frequency Diversity-cont’d
 Frequency Diversity uses separate
frequencies (dual transmit and receive
systems); it monitors primary for fail
over and switches to standby.
Interference usually affects only one
range of frequencies. Not allowed in
non-carrier applications because of
spectrum scarcity.
Hot Standby*
Receiver
System XTMR
Primary #1
System XTMR
Standby #2
failure switch
Active RCVR
#1
Standby RCVR
#2
Transmitter
*Hot standby is designed for equipment failure only
PRI
ReceiverTransmitter
Connect to
PRI interface
& PSTN
Connect to
PRI interface
& PSTN
To PSTN To PSTN
System
Transmission
Facilities
System
Receiver
Facilities
Availability Formula
Percent Availability equals:
1 – (outage hours/8760 hours per year)
Private microwaves have 99.99% availability
Microwave Path Analysis
 Transmitter output power
 Antenna gain
 proportional to the physical characteristics
of the antenna (diameter)
 Free space gain
 Antenna alignment factor
 Unfaded received signal level
Microwave Radio Applications
Satellite Communications
Satellite-Related Terms
 Earth Stations – antenna systems on or near earth
 Uplink – transmission from an earth station to a
satellite
 Downlink – transmission from a satellite to an
earth station
 Transponder – electronics in the satellite that
convert uplink signals to downlink signals
Ways to Categorize
Communications Satellites
 Coverage area
 Global, regional, national
 Service type
 Fixed service satellite (FSS)
 Broadcast service satellite (BSS)
 Mobile service satellite (MSS)
 General usage
 Commercial, military, amateur, experimental
Classification of Satellite Orbits
 Circular or elliptical orbit
 Circular with center at earth’s center
 Elliptical with one foci at earth’s center
 Orbit around earth in different planes
 Equatorial orbit above earth’s equator
 Polar orbit passes over both poles
 Other orbits referred to as inclined orbits
 Altitude of satellites
 Geostationary orbit (GEO)
 Medium earth orbit (MEO)
 Low earth orbit (LEO)
Geometry Terms
 Elevation angle - the angle from the
horizontal to the point on the center of the
main beam of the antenna when the antenna
is pointed directly at the satellite
 Minimum elevation angle
 Coverage angle - the measure of the portion
of the earth's surface visible to the satellite
Minimum Elevation Angle
 Reasons affecting minimum elevation angle
of earth station’s antenna (>0o
)
 Buildings, trees, and other terrestrial objects
block the line of sight
 Atmospheric attenuation is greater at low
elevation angles
 Electrical noise generated by the earth's heat
near its surface adversely affects reception
GEO Orbit
 Advantages of the the GEO orbit
 No problem with frequency changes
 Tracking of the satellite is simplified
 High coverage area
 Disadvantages of the GEO orbit
 Weak signal after traveling over 35,000 km
 Polar regions are poorly served
 Signal sending delay is substantial
LEO Satellite Characteristics
 Circular/slightly elliptical orbit under 2000 km
 Orbit period ranges from 1.5 to 2 hours
 Diameter of coverage is about 8000 km
 Round-trip signal propagation delay less than 20
ms
 Maximum satellite visible time up to 20 min
 System must cope with large Doppler shifts
 Atmospheric drag results in orbital deterioration
LEO Categories
 Little LEOs
 Frequencies below 1 GHz
 5MHz of bandwidth
 Data rates up to 10 kbps
 Aimed at paging, tracking, and low-rate messaging
 Big LEOs
 Frequencies above 1 GHz
 Support data rates up to a few megabits per sec
 Offer same services as little LEOs in addition to voice
and positioning services
MEO Satellite Characteristics
 Circular orbit at an altitude in the range of 5000 to
12,000 km
 Orbit period of 6 hours
 Diameter of coverage is 10,000 to 15,000 km
 Round trip signal propagation delay less than 50
ms
 Maximum satellite visible time is a few hours
Frequency Bands Available for
Satellite Communications
Satellite Link Performance Factors
 Distance between earth station antenna and
satellite antenna
 For downlink, terrestrial distance between earth
station antenna and “aim point” of satellite
 Displayed as a satellite footprint (Figure 9.6)
 Atmospheric attenuation
 Affected by oxygen, water, angle of elevation, and
higher frequencies
Satellite Footprint
Satellite Network Configurations
Capacity Allocation Strategies
 Frequency division multiple access
(FDMA)
 Time division multiple access (TDMA)
 Code division multiple access (CDMA)
Frequency-Division Multiplexing
 Alternative uses of channels in point-to-point
configuration
 1200 voice-frequency (VF) voice channels
 One 50-Mbps data stream
 16 channels of 1.544 Mbps each
 400 channels of 64 kbps each
 600 channels of 40 kbps each
 One analog video signal
 Six to nine digital video signals
Frequency-Division Multiple
Access
 Factors which limit the number of
subchannels provided within a satellite
channel via FDMA
 Thermal noise
 Intermodulation noise
 Crosstalk
Forms of FDMA
 Fixed-assignment multiple access (FAMA)
 The assignment of capacity is distributed in a fixed
manner among multiple stations
 Demand may fluctuate
 Results in the significant underuse of capacity
 Demand-assignment multiple access (DAMA)
 Capacity assignment is changed as needed to respond
optimally to demand changes among the multiple
stations
FAMA-FDMA
 FAMA – logical links between stations are
preassigned
 FAMA – multiple stations access the
satellite by using different frequency bands
 Uses considerable bandwidth
DAMA-FDMA
 Single channel per carrier (SCPC) – bandwidth
divided into individual VF channels
 Attractive for remote areas with few user stations near
each site
 Suffers from inefficiency of fixed assignment
 DAMA – set of subchannels in a channel is treated
as a pool of available links
 For full-duplex between two earth stations, a pair of
subchannels is dynamically assigned on demand
 Demand assignment performed in a distributed fashion
by earth station using CSC
Reasons for Increasing Use of TDM
Techniques
 Cost of digital components continues to
drop
 Advantages of digital components
 Use of error correction
 Increased efficiency of TDM
 Lack of intermodulation noise
FAMA-TDMA Operation
 Transmission in the form of repetitive sequence of
frames
 Each frame is divided into a number of time slots
 Each slot is dedicated to a particular transmitter
 Earth stations take turns using uplink channel
 Sends data in assigned time slot
 Satellite repeats incoming transmissions
 Broadcast to all stations
 Stations must know which slot to use for
transmission and which to use for reception
FAMA-TDMA Uplink
FAMA-TDMA Downlink

microwave

  • 1.
    Fundamentals of Microwave& Satellite Technologies
  • 2.
    Historical Perspective  Foundedduring WWII  Used for long-haul telecommunications  Displaced by fiber optic networks  Still viable for right-of-way bypass and geographic obstruction avoidance
  • 3.
    Microwave Spectrum  Rangeis approximately 1 GHz to 40 GHz  Total of all usable frequencies under 1 GHz gives a reference on the capacity of in the microwave range
  • 4.
    Microwave Impairments  Equipment,antenna, and waveguide failures  Fading and distortion from multipath reflections  Absorption from rain, fog, and other atmospheric conditions  Interference from other frequencies
  • 5.
    Microwave Engineering Considerations  Freespace & atmospheric attenuation  Reflections  Diffractions  Rain attenuation
  • 6.
    Microwave Engineering Considerations-cont’d  Skinaffect  Line of Sight (LOS)  Fading  Range  Interference
  • 7.
    Free Space &Atmospheric Attenuation  Free space & atmospheric attenuation is defined by the loss the signal undergoes traveling through the atmosphere. Changes in air density and absorption by atmospheric particles.
  • 8.
    Reflections  Reflections canoccur as the microwave signal traverses a body of water or fog bank; cause multipath conditions
  • 9.
    Diffraction  Diffraction isthe result of variations in the terrain the signal crosses
  • 10.
    Rain Attenuation  Raindropabsorption or scattering of the microwave signal can cause signal loss in transmissions.
  • 11.
    Skin Affect  SkinAffect is the concept that high frequency energy travels only on the outside skin of a conductor and does not penetrate into it any great distance. Skin Affect determines the properties of microwave signals.
  • 12.
    Line of Sight FresnelZone Clearance  Fresnel Zone Clearance is the minimum clearance over obstacles that the signal needs to be sent over. Reflection or path bending will occur if the clearance is not sufficient.
  • 13.
    LOS & FZC-cont’d FresnelZone D1 D2 72.2 D1 X D2 F x D secret formula
  • 14.
    Microwave Fading Normal Signal ReflectivePath Caused by multi-path reflections and heavy rains
  • 15.
    Range  The distancea signal travels and its increase in frequency are inversely proportional  Repeaters extend range  Back-to-back antennas  reflectors
  • 16.
    Range-cont’d  High frequenciesare repeated/received at or below one mile  Lower frequencies can travel up to 100 miles but 25-30 miles is the typical placement for repeaters
  • 17.
    Interference  Adjacent ChannelInterference  digital not greatly affected  Overreach  caused by signal feeding past a repeater to the receiving antenna at the next station in the route. Eliminated by zigzag path alignment or alternate frequency use between adjacent stations
  • 18.
    Components of aMicrowave System  Digital Modem  Radio Frequency (RF) Unit  Antenna
  • 19.
    Digital Modem  Thedigital modem modulates the information signal (intermediate frequency or IF).
  • 20.
    RF Unit  IFis fed to the RF unit which is mounted as close physically to the antenna as possible (direct connect is optimal).
  • 21.
    Antenna  The antennais a passive device that radiates the modulated signal. It is fed by direct connect of the RF unit, coaxial cable, or waveguides at higher frequencies.
  • 22.
    Waveguides Waveguides are hollowchannels of low-loss material used to direct the signal from the RF unit to the antenna.
  • 23.
    Modulation Methods  Primarilymodulated today with digital FM or AM signals  Digital signal remains quiet until failure threshold bit error rate renders it unusable
  • 24.
    Bit Error Rate(BER)  The BER is a performance measure of microwave signaling throughput  10 or one error per million transmitted bits of information  Data fail over is at 10 ; voice traffic can withstand this error rate -6 -3
  • 25.
    Diversity  Space Diversity Frequency Diversity  Hot Standby  PRI
  • 26.
    Space Diversity Normal Signal FadedSignal Transmitter Receiver
  • 27.
    Space Diversity-cont’d  SpaceDiversity protects against multi- path fading by automatic switch over to another antenna place below the primary antenna. This is done at the BER failure point or signal strength attenuation point to the secondary antenna that is receiving the transmitted signal at a stronger power rating.
  • 28.
    Frequency Diversity Receiver Active XTMR Frequency#1 Protect XTMR Frequency #2 RCVR Frequency #1 RCVR Frequency #2 Transmitter
  • 29.
    Frequency Diversity-cont’d  FrequencyDiversity uses separate frequencies (dual transmit and receive systems); it monitors primary for fail over and switches to standby. Interference usually affects only one range of frequencies. Not allowed in non-carrier applications because of spectrum scarcity.
  • 30.
    Hot Standby* Receiver System XTMR Primary#1 System XTMR Standby #2 failure switch Active RCVR #1 Standby RCVR #2 Transmitter *Hot standby is designed for equipment failure only
  • 31.
    PRI ReceiverTransmitter Connect to PRI interface &PSTN Connect to PRI interface & PSTN To PSTN To PSTN System Transmission Facilities System Receiver Facilities
  • 32.
    Availability Formula Percent Availabilityequals: 1 – (outage hours/8760 hours per year) Private microwaves have 99.99% availability
  • 33.
    Microwave Path Analysis Transmitter output power  Antenna gain  proportional to the physical characteristics of the antenna (diameter)  Free space gain  Antenna alignment factor  Unfaded received signal level
  • 34.
  • 39.
  • 40.
    Satellite-Related Terms  EarthStations – antenna systems on or near earth  Uplink – transmission from an earth station to a satellite  Downlink – transmission from a satellite to an earth station  Transponder – electronics in the satellite that convert uplink signals to downlink signals
  • 41.
    Ways to Categorize CommunicationsSatellites  Coverage area  Global, regional, national  Service type  Fixed service satellite (FSS)  Broadcast service satellite (BSS)  Mobile service satellite (MSS)  General usage  Commercial, military, amateur, experimental
  • 42.
    Classification of SatelliteOrbits  Circular or elliptical orbit  Circular with center at earth’s center  Elliptical with one foci at earth’s center  Orbit around earth in different planes  Equatorial orbit above earth’s equator  Polar orbit passes over both poles  Other orbits referred to as inclined orbits  Altitude of satellites  Geostationary orbit (GEO)  Medium earth orbit (MEO)  Low earth orbit (LEO)
  • 43.
    Geometry Terms  Elevationangle - the angle from the horizontal to the point on the center of the main beam of the antenna when the antenna is pointed directly at the satellite  Minimum elevation angle  Coverage angle - the measure of the portion of the earth's surface visible to the satellite
  • 44.
    Minimum Elevation Angle Reasons affecting minimum elevation angle of earth station’s antenna (>0o )  Buildings, trees, and other terrestrial objects block the line of sight  Atmospheric attenuation is greater at low elevation angles  Electrical noise generated by the earth's heat near its surface adversely affects reception
  • 45.
    GEO Orbit  Advantagesof the the GEO orbit  No problem with frequency changes  Tracking of the satellite is simplified  High coverage area  Disadvantages of the GEO orbit  Weak signal after traveling over 35,000 km  Polar regions are poorly served  Signal sending delay is substantial
  • 46.
    LEO Satellite Characteristics Circular/slightly elliptical orbit under 2000 km  Orbit period ranges from 1.5 to 2 hours  Diameter of coverage is about 8000 km  Round-trip signal propagation delay less than 20 ms  Maximum satellite visible time up to 20 min  System must cope with large Doppler shifts  Atmospheric drag results in orbital deterioration
  • 47.
    LEO Categories  LittleLEOs  Frequencies below 1 GHz  5MHz of bandwidth  Data rates up to 10 kbps  Aimed at paging, tracking, and low-rate messaging  Big LEOs  Frequencies above 1 GHz  Support data rates up to a few megabits per sec  Offer same services as little LEOs in addition to voice and positioning services
  • 48.
    MEO Satellite Characteristics Circular orbit at an altitude in the range of 5000 to 12,000 km  Orbit period of 6 hours  Diameter of coverage is 10,000 to 15,000 km  Round trip signal propagation delay less than 50 ms  Maximum satellite visible time is a few hours
  • 49.
    Frequency Bands Availablefor Satellite Communications
  • 50.
    Satellite Link PerformanceFactors  Distance between earth station antenna and satellite antenna  For downlink, terrestrial distance between earth station antenna and “aim point” of satellite  Displayed as a satellite footprint (Figure 9.6)  Atmospheric attenuation  Affected by oxygen, water, angle of elevation, and higher frequencies
  • 51.
  • 52.
  • 53.
    Capacity Allocation Strategies Frequency division multiple access (FDMA)  Time division multiple access (TDMA)  Code division multiple access (CDMA)
  • 54.
    Frequency-Division Multiplexing  Alternativeuses of channels in point-to-point configuration  1200 voice-frequency (VF) voice channels  One 50-Mbps data stream  16 channels of 1.544 Mbps each  400 channels of 64 kbps each  600 channels of 40 kbps each  One analog video signal  Six to nine digital video signals
  • 55.
    Frequency-Division Multiple Access  Factorswhich limit the number of subchannels provided within a satellite channel via FDMA  Thermal noise  Intermodulation noise  Crosstalk
  • 56.
    Forms of FDMA Fixed-assignment multiple access (FAMA)  The assignment of capacity is distributed in a fixed manner among multiple stations  Demand may fluctuate  Results in the significant underuse of capacity  Demand-assignment multiple access (DAMA)  Capacity assignment is changed as needed to respond optimally to demand changes among the multiple stations
  • 57.
    FAMA-FDMA  FAMA –logical links between stations are preassigned  FAMA – multiple stations access the satellite by using different frequency bands  Uses considerable bandwidth
  • 58.
    DAMA-FDMA  Single channelper carrier (SCPC) – bandwidth divided into individual VF channels  Attractive for remote areas with few user stations near each site  Suffers from inefficiency of fixed assignment  DAMA – set of subchannels in a channel is treated as a pool of available links  For full-duplex between two earth stations, a pair of subchannels is dynamically assigned on demand  Demand assignment performed in a distributed fashion by earth station using CSC
  • 59.
    Reasons for IncreasingUse of TDM Techniques  Cost of digital components continues to drop  Advantages of digital components  Use of error correction  Increased efficiency of TDM  Lack of intermodulation noise
  • 60.
    FAMA-TDMA Operation  Transmissionin the form of repetitive sequence of frames  Each frame is divided into a number of time slots  Each slot is dedicated to a particular transmitter  Earth stations take turns using uplink channel  Sends data in assigned time slot  Satellite repeats incoming transmissions  Broadcast to all stations  Stations must know which slot to use for transmission and which to use for reception
  • 61.
  • 62.