Mobile Communications
Chapter 5: Satellite Systems
History
 Basics
 Orbits
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Mobile Communications
LEO, MEO, GEO
 Examples
 Handover, Routing
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Satellite Systems
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History of satellite communication
1945
1957
1960
1963
1965
1976
1982
1988
1993
1998
Arthur C. Clarke publishes an essay about „Extra
Terrestrial Relays“
first satellite SPUTNIK
first reflecting communication satellite ECHO
first geostationary satellite SYNCOM
first commercial geostationary satellite Satellit „Early Bird“
(INTELSAT I): 240 duplex telephone channels or 1 TV
channel, 1.5 years lifetime
three MARISAT satellites for maritime communication
first mobile satellite telephone system INMARSAT-A
first satellite system for mobile phones and data
communication INMARSAT-C
first digital satellite telephone system
global satellite systems for small mobile phones
Mobile Communications
Satellite Systems
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Applications
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Traditionally
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weather satellites
radio and TV broadcast satellites
military satellites
satellites for navigation and localization (e.g., GPS)
Telecommunication
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global telephone connections
replaced by fiber optics
backbone for global networks
connections for communication in remote places or underdeveloped areas
global mobile communication
 satellite systems to extend cellular phone systems
Mobile Communications
Satellite Systems
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Classical satellite systems
Inter Satellite Link
(ISL)
Mobile User
Link (MUL)
MUL
Gateway Link
(GWL)
GWL
small cells
(spotbeams)
base station
or gateway
footprint
ISDN
PSTN: Public Switched
Telephone Network
GSM
PSTN
User data
Mobile Communications
Satellite Systems
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Basics
Satellites in circular orbits
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attractive force Fg = m g (R/r)²
centrifugal force Fc = m r ω²
m: mass of the satellite
R: radius of the earth (R = 6370 km)
r: distance to the center of the earth
g: acceleration of gravity (g = 9.81 m/s²)
ω: angular velocity (ω = 2 π f, f: rotation frequency)
Stable orbit
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Fg = Fc
r=3
gR 2
(2π f ) 2
Mobile Communications
Satellite Systems
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Satellite period and orbits
24
satellite
period [h]
velocity [ x1000 km/h]
20
16
12
8
4
synchronous distance
35,786 km
10
20
30
40 x106 m
radius
Mobile Communications
Satellite Systems
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Basics
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elliptical or circular orbits
complete rotation time depends on distance satellite-earth
inclination: angle between orbit and equator
elevation: angle between satellite and horizon
LOS (Line of Sight) to the satellite necessary for connection
 high elevation needed, less absorption due to e.g. buildings
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Uplink: connection base station - satellite
Downlink: connection satellite - base station
typically separated frequencies for uplink and downlink
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transponder used for sending/receiving and shifting of frequencies
transparent transponder: only shift of frequencies
regenerative transponder: additionally signal regeneration
Mobile Communications
Satellite Systems
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Inclination
plane of satellite orbit
satellite orbit
perigee
δ
inclination δ
equatorial plane
Mobile Communications
Satellite Systems
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Elevation
Elevation:
angle ε between center of satellite beam
and surface
minimal elevation:
elevation needed at least
to communicate with the satellite
Mobile Communications
ε
Satellite Systems
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Link budget of satellites
Parameters like attenuation or received power determined by four
parameters:
L: Loss
 sending power
f: carrier frequency
 gain of sending antenna
r: distance
c: speed of light
 distance between sender
2
and receiver
 4π r f 
L=
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 gain of receiving antenna
 c 
Problems
 varying strength of received signal due to multipath propagation
 interruptions due to shadowing of signal (no LOS)
Possible solutions
 Link Margin to eliminate variations in signal strength
 satellite diversity (usage of several visible satellites at the same time)
helps to use less sending power
Mobile Communications
Satellite Systems
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Atmospheric attenuation
Attenuation of
the signal in %
Example: satellite systems at 4-6 GHz
50
40
rain absorption
30
fog absorption
ε
20
10
atmospheric
absorption
5° 10°
20°
30°
40°
50°
elevation of the satellite
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Satellite Systems
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Orbits I
Four different types of satellite orbits can be identified depending
on the shape and diameter of the orbit:
 GEO: geostationary orbit, ca. 36000 km above earth surface
 LEO (Low Earth Orbit): ca. 500 - 1500 km
 MEO (Medium Earth Orbit) or ICO (Intermediate Circular Orbit):
ca. 6000 - 20000 km
 HEO (Highly Elliptical Orbit) elliptical orbits
Mobile Communications
Satellite Systems
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Orbits II
GEO (Inmarsat, Thuraya)
HEO
MEO (ICO, GPS)
LEO
(Globalstar,
Irdium)
inner and outer Van
Allen belts
earth
1000
10000
Van-Allen-Belts:
ionized particles
2000 - 6000 km and
15000 - 30000 km
above earth surface
Mobile Communications
35768
km
Satellite Systems
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LEO systems
Orbit ca. 500 - 1500 km above earth surface
 visibility of a satellite ca. 10 - 40 minutes
 global radio coverage possible
 latency comparable with terrestrial long distance
connections, ca. 5 - 10 ms
 smaller footprints, better frequency reuse
 but now handover necessary from one satellite to another
 many satellites necessary for global coverage
 more complex systems due to moving satellites
Examples:
Iridium (start 1998, 66 satellites)
 Globalstar (start 2000, 48 satellites)
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Mobile Communications
Satellite Systems
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Satellite Systems
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MEO systems
Orbit ca. 5000 - 12000 km above earth surface
comparison with LEO systems:
 slower moving satellites
 less satellites needed
 simpler system design
 for many connections no hand-over needed
 higher latency, ca. 70 - 80 ms
 higher sending power needed
 special antennas for small footprints needed
Example:
 ICO (Intermediate Circular Orbit, Inmarsat)
 GPS, GALILEO
Mobile Communications
MEO systems: GPS (Global Positioning System)
Basic concept of GPS
 GPS receiver calculates its position (latitude, longitude, and altitude) by
precisely timing the signals sent by GPS satellites high above the Earth
 Each satellite continually transmits messages that include
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the time the message was transmitted
precise orbital information
the general system health and rough orbits of all GPS satellites
Receiver uses the received messages to determine the transit time of
each message and computes the distance to each satellite
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Trilateration
Due to errors (inprecise clocks), not three but four or more satellites are
used for calculations
Position useful in mobil communications for “Location based services”
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Accuracy: „some meter“ with Wide Area Augmentation System WAAS
Adopted from Wikipedia
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Satellite Systems
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MEO systems: GPS (Global Positioning System)
Structure: three major segments
1. space segment (SS)
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2.
control segment (CS)
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3.
orbiting GPS satellites, or Space Vehicles (SV)
master control station (MCS),
alternate master control station,
four dedicated ground antennas and
six dedicated monitor stations
user segment (U.S.)
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user devices
US Air Force develops, maintains, and operates space & ctrl segments
Adopted from Wikipedia
Mobile Communications
Satellite Systems
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MEO systems: GPS (Global Positioning System)
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Space segment (SS)
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orbiting GPS satellites, or Space Vehicles (SV)
24 SVs: six planes with four satellites each (plus some extra)
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approximately 55° inclination
orbits are arranged such that >= 6 satellites are always within LOS
 four satellites are not evenly spaced (90 degrees) within each orbit,
but 30, 105, 120, and 105 degrees
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rotation time approx. 12 hours
orbit 20200 km
~ 9 satellites are visible from any point on ground at any one time
Mobile Communications
Satellite Systems
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MEO systems: GPS (Global Positioning System)
Ground-Track (sub satellite path) of the Satellite GPS BIIR-07 (PRN 18)
•
of 18.10.2001, 00:00 h
to 19.10.2001, 00:00 h
•
orbit time is slightly shifted (about 4 minutes) in 24 h
•
21:30
zone of sight
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Satellite Systems
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MEO systems: GPS (Global Positioning System)
Position of the monitor stations and the master control station
(Earthmap:NASA; http://visibleearth.nasa.gov/)
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“master control station” (Schriever AFB)
plus additional monitoring stations for monitoring the satellites
every satellite can be seen from at least two monitor stations
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Satellite Systems
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Geostationary satellites
Orbit 35,786 km distance to earth surface, orbit in equatorial plane
(inclination 0°)
 complete rotation exactly one day, satellite is synchronous to earth
rotation
 fix antenna positions, no adjusting necessary
 satellites typically have a large footprint (up to 34% of earth surface!),
therefore difficult to reuse frequencies
 bad elevations in areas with latitude above 60° due to fixed position
above the equator
 high transmit power needed
 high latency due to long distance (ca. 275 ms)
 not useful for global coverage for small mobile phones and data
transmission, typically used for radio and TV transmission, but some
for mobile communications as well
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Satellite Systems
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GEO Systems: Example Thuraya
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regional satellite phone provider
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shareholders are mixture of Middle Eastern and North African telcos and
investment companies
coverage area most of Europe, Middle East, North, Central and East
Africa, Asia and Australia
subscribers:
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~ 250,000 (March 2006)
~ 360,000 Thuraya handsets in service since launch in 2001
Structure of Thuraya spot beams
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Satellite Systems
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GEO Systems: Example Thuraya
Mobile Communications
Satellite Systems
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GEO Systems: Example Thuraya
Services
• Voice communications with hand held or fixed terminals
• Short message service
• 9.6 kbit/s of data & fax service
• 60 kbit/s downlink and 15 kbit/s uplink "GMPRS" mobile data service
• 144 kbit/s high-speed data transfer via a notebook-sized terminal
(ThurayaDSL)
• GPS is supported by all handsets
• value-added services, e.g., news, call back / waiting, missed calls
• one-way 'high power alert' capability that notifies users of incoming
call, when signal path to satellite is obstructed (e.g. inside building)
• Marine Services: a combination of a special (fixed) base station and
subscription offering voice, fax, data and always on internet-access
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Also an emergency service: sends multiple SMS messages containing alarm-status
and actual position to pre-defined destinations
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Satellite Systems
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GEO Systems: Example SkyDSL
Internet access via satellite
 Interesting for users in areas
where no other broadband Internet
access available
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has technically not much to do with DSL
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GEO satellite for downlink
uplink (also for requests) via modem/telephone or other mobil comm.
or also via satellite
data rate up to max. 36000 KBit/s
# users
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large latency due to GEO
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ca. 100.000 in Germany
already signal propagation for distance of 2 * 36000 km: ~240 ms
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Satellite Systems
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Routing
One solution: inter satellite links (ISL)
 reduced number of gateways needed
 forward connections or data packets within the satellite network as long
as possible
 only one uplink and one downlink per direction needed for the
connection of two mobile phones
Problems:
 more complex focusing of antennas between satellites
 high system complexity due to moving routers
 higher fuel consumption
 thus shorter lifetime
Iridium and Teledesic planned with ISL
Other systems use gateways and additionally terrestrial networks
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Satellite Systems
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Localization of mobile stations
Mechanisms similar to GSM
Gateways maintain registers with user data
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HLR (Home Location Register): static user data
VLR (Visitor Location Register): (last known) location of the mobile station
SUMR (Satellite User Mapping Register):
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satellite assigned to a mobile station
positions of all satellites
Registration of mobile stations
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Localization of the mobile station via the satellite’s position
requesting user data from HLR
updating VLR and SUMR
Calling a mobile station
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localization using HLR/VLR similar to GSM
connection setup using the appropriate satellite
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Satellite Systems
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Handover in satellite systems
Several additional situations for handover in satellite systems
compared to cellular terrestrial mobile phone networks caused
by the movement of the satellites
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Intra satellite handover
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Inter satellite handover
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handover from one satellite to another satellite
mobile station leaves the footprint of one satellite
Gateway handover
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handover from one spot beam to another
mobile station still in the footprint of the satellite, but in another cell
Handover from one gateway to another
mobile station still in the footprint of a satellite, but gateway leaves the
footprint
Inter system handover
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Handover from the satellite network to a terrestrial cellular network
mobile station can reach a terrestrial network again which might be
cheaper, has a lower latency etc.
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Satellite Systems
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