study

1. Fundamentals of Microwave &
Satellite Technologies
TEL 117
Telekomunikasi Dasar

2. 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

3. 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

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
 Free space &
atmospheric
attenuation
 Reflections
 Diffractions
 Rain attenuation
 Skin affect
 Line of Sight (LOS)
 Fading
 Range
 Interference

6. 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.

7. Reflections
 Reflections can occur as the microwave
signal traverses a body of water or fog
bank; cause multipath conditions

8. Diffraction
 Diffraction is the result of variations in
the terrain the signal crosses

9. Rain Attenuation
 Raindrop absorption or scattering of the
microwave signal can cause signal loss
in transmissions.

10. 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.

11. 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.

12. LOS & FZC-cont’d
Fresnel Zone
D1
D2
72.2
D1 X D2
F x D
secret formula

13. Microwave Fading
Normal Signal
Reflective Path
Caused by multi-path reflections and heavy rains

14. Range
 The distance a signal travels and its
increase in frequency are inversely
proportional
 Repeaters extend range
 Back-to-back antennas
 Reflectors

15. 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

16. 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

17. Components of a Microwave
System
 Digital Modem
 Radio Frequency (RF) Unit
 Antenna

18. Digital Modem
 The digital modem modulates the
information signal (intermediate
frequency or IF).

19. RF Unit
 IF is fed to the RF unit which is
mounted as close physically to the
antenna as possible (direct connect is
optimal).

20. 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.

21. Waveguides
Waveguides are hollow channels of
low-loss material used to direct the
signal from the RF unit to the
antenna.

22. Modulation Methods
 Primarily modulated today with digital
FM or AM signals
 Digital signal remains quiet until failure
threshold bit error rate renders it unusable

23. 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

24. Diversity
 Space Diversity
 Frequency Diversity
 Hot Standby
 PRI

25. Space Diversity
Normal Signal
Faded Signal
Transmitter Receiver

26. 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.

27. Frequency Diversity
Receiver
Active Tx
Frequency #1
Protect Tx
Frequency #2
Rx
Frequency #1
Rx
Frequency #2
Transmitter

28. 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.

29. Hot Standby*
Receiver
System Tx
Primary #1
System Tx
Standby #2
failure switch
Active Rx
#1
Standby Rx
#2
Transmitter
*Hot standby is designed for equipment failure only

30. PRI (Primary Rate Interface)
ReceiverTransmitter
Connect to
PRI interface
& PSTN
Connect to
PRI interface
& PSTN
To PSTN To PSTN
System
Transmission
Facilities
System
Receiver
Facilities
PRI is an ISDN service providing user with 23,64 kbps for channel message and 1,64
kbps data channel for control & signalling. PRI is ISDN E1 interface.

31. Availability Formula
Percent Availability equals:
1 – (outage hours/8760 hours per year)
Private microwaves have 99.99% availability

32. 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

33. Microwave Radio Applications

38. Satellite Communications

39. 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

40. 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

41. 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)

42. 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

43. 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

44. 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
GEO : Geosynchronous equatorial orbit

45. 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 : Low earth orbit

46. 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

47. 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
MEO : Medium Earth Orbit

48. Satellite Systems
SOURCE: WASHINGTON UNIV.
GEO
M EO
LEO
GEO (22,300 mi., equatorial)
high bandwidth, power, latency
MEO
high bandwidth, power, latency
LEO (400 mi.)
low power, latency
more satellites
small footprint
V-SAT (Very Small Aperture
Terminal)
private WAN
SATELLITE MAP

49. Geostationary Orbit
SOURCE: BILL LUTHER, FCC

50. GPS Satellite Constellation
• Global Positioning
System
• Operated by USAF
• 28 satellites
• 6 orbital planes at a
height of 20,200 km
• Positioned so a
minimum of 5 satellites
are visible at all times
• Receiver measures
distance to satellite
SOURCE: NAVSTAR

51. Frequency Bands Available for
Satellite Communications

52. 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

53. Satellite Footprint

54. Satellite Network Configurations

55. Capacity Allocation Strategies
 Frequency division multiple access
(FDMA)
 Time division multiple access (TDMA)
 Code division multiple access (CDMA)

56. 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

57. Frequency-Division Multiple
Access
 Factors which limit the number of
subchannels provided within a satellite
channel via FDMA
 Thermal noise
 Intermodulation noise
 Crosstalk

58. 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

59. FAMA-FDMA
 FAMA – logical links between stations are
preassigned
 FAMA – multiple stations access the
satellite by using different frequency bands
 Uses considerable bandwidth

60. 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

61. 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

62. 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

63. FAMA-TDMA Uplink

64. FAMA-TDMA Downlink