TELIT GROUP Industries for Telecommunicati 1 2 7 t h F e b r u a r y 2 0 0 1 Satellite Personal Communications Systems (S-PCS): the Globalstar System and evolutionary paths towards 3G SCHOOL ON DIGITAL AND MULTIMEDIA COMMUNICATIONS USING TERRESTRIAL AND SATELLITE RADIO LINKS TELIT MOBILE TERMINALS Giovanni De Maio Telit Mobile Terminals S.p.A. Project Manager - System Engineering Satellite User Terminal Division Via Vitorchiano, 81 - Rome [email protected]
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TELIT GROUP Industries for Telecommunications 1 27th February 2001 Satellite Personal Communications Systems (S-PCS): the Globalstar System and evolutionary.
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TELIT GROUP Industries for Telecommunications 1
27th F
ebru
ary 2001
Satellite Personal Communications Systems (S-PCS):
the Globalstar System and evolutionary paths towards 3G
SCHOOL ON DIGITAL
AND MULTIMEDIA
COMMUNICATIONS
USING TERRESTRIAL
AND SATELLITE
RADIO LINKSTELIT MOBILE TERMINALS
Giovanni De MaioTelit Mobile Terminals S.p.A.Project Manager - System EngineeringSatellite User Terminal DivisionVia Vitorchiano, 81 - [email protected]
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Globalstar System Overview
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Globalstar is a system that provide digital telephony with a global coverage, by means of a satellite constellation working in a Low Earth Orbit (LEO).
Globalstar allows access to the terrestrial networks, both fixed and mobile, interworking with them in a complementary way.
In areas not covered by the terrestrial networks, the Globalstar Terminal can be set to switch automatically from the terrestrial to the satellite mode.
The system is designed in order to maximise coverage in the temperate areas.
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Globalstar service aspects
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Gateway
Mobile Portable Fixed
Space Segment
User Segment
Ground Segment
Terrestrial NetworkPLMN/PSTN
GBO
GDN
SOCC
GOCC
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Globalstar System Architecture
GOCC: Ground Operations Control Center
SOCC: Space Operations Control Center
GDN: Globalstar Data Network
GBO: Globalstar Business Office
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Globalstar constellation
At least 7.5 years life time
Weight: 450 Kg
1100 Watts against 2000 circuits
Distance 1414 Km at 52°
8 orbital planes e 6 equally spaced satellites per orbit
Circular orbit period 113 minutes
48 LEO satellites:
User terminals can be served by a satellite 10 to 15 minutes out of each orbit.
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Space Segment
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Earth Surface Coverage
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Space Segment
The system is designed in order to maximise coverage in the temperate areas.
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Multiple Coverage (48 SATELLITES; 10° ELEVATION)
At LATITUDE 40°:
At least 4 satellites for 38% of time
At least 3 satellites for 87% of time
At least 2 satellites always visible
At least one satellite always visible for LATITUDE<70°
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Space Segment
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immagini
immagini
User and feeder links
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Space Segment
Satellites are of the non regenerative type: they simply perform a transparent relay of the signals in both Forward and Reverse links
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Space SegmentFrequency channels G
lob
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Space Segment
1 . 2 3 M H z 1 . 2 3 M H z 1 . 2 3 M H z 1 . 2 3 M H z 1 . 2 3 M H z 1 . 2 3 M H z 1 . 2 3 M H z
1 6 2 6 . 5 M H z
1 6 2 5 . 4 9 0 M H z
1 6 1 0 . 0 M H z
7 3 0 k H z
1 6 2 4 . 2 6 0 M H z
1 6 2 3 . 0 3 0 M H z
1 6 2 1 . 8 0 0 M H z
1 6 2 0 . 5 7 0 M H z
1 6 1 9 . 3 4 0 M H z
1 6 1 8 . 1 1 0 M H z
1 6 1 6 . 8 8 0 M H z
1 6 1 5 . 6 5 0 M H z
1 6 1 4 . 4 2 0 M H z
1 6 1 3 . 1 9 0 M H z
1 6 1 1 . 9 6 0 M H z
1 6 1 0 . 7 3 0 M H z
1 6 . 5 M H z F i l e : L - B a n d
1 0 1 0 k H z
1 2 3 4 5 6 7 8 9 1 0 1 1 1 2 1 3
2 5 0 0 . 0 M H z
2 4 9 9 . 1 5 0 M H z
2 4 8 3 . 5 M H z
2 4 9 7 . 9 2 0 M H z
2 4 9 6 . 6 9 0 M H z
2 4 9 5 . 4 6 0 M H z
2 4 9 4 . 2 3 0 M H z
2 4 9 3 . 0 0 0 M H z
2 4 9 1 . 7 7 0 M H z
2 4 9 0 . 5 4 0 M H z
2 4 8 9 . 3 1 0 M H z
2 4 8 8 . 0 8 0 M H z
2 4 8 6 . 8 5 0 M H z
2 4 8 5 . 6 2 0 M H z
2 4 8 4 . 3 9 0 M H z
1 . 2 3 M H z 1 . 2 3 M H z 1 . 2 3 M H z 1 . 2 3 M H z 1 . 2 3 M H z 1 . 2 3 M H z 1 . 2 3 M H z
8 9 0 k H z
1 6 . 5 M H z F i l e : S - B a n d
8 5 0 k H z
1 2 3 4 5 6 7 8 9 1 0 1 1 1 2 1 3
Forward and Reverse User links channels or Sub-Beams
S-Band Forward User Linkchannels (Sub-Beams)
L-Band Reverse User Link channels (Sub-Beams)
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Space Segment Sub-Beams to Gateways Assignment
Overlapping Beams will transmit Sub-Beams for both Gateways
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Space Segment Glo
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PILOT: unmodulated DS SS signal transmitted by the Gateway (employed to acquire the timing, as phase reference for demodulation and to handoff)
SYNC: channel carrying a repeating message for terminal synchronization
PAGING:
provides system access information for registering UT’s
lets a phone know that a call is coming in or that there is a message in voice mail
for SMS
to reply to a UT trying to place a call, for handoff messaging when not in a call
TRAFFIC: communication path between a UT and a Gateway, which implies a Forward and a Reverse Traffic Channel pair; for voice, data, signaling (when in a call)
ACCESS: slotted random access channel for call originations, responses to pages and registrations
Globalstar Air Interface Channels
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Space Segment Glo
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Example of a Forward CDMA Channel
The above example shows a particular assignment of the overall 128 channels (codes)
within a 1.23 MHz Forward Channel to Pilot, Sync, Paging and Traffic functionalities
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Space Segment
Acquisition Search Space
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pilot signal in a three dimensional search space: its
dimensions are PN Code, PN Timing and Frequency
Doppler Shift. Note that the Frequency Doppler Shift
is actually a quite minor issue for acquisition in a
terrestrial environment (e.g. IS-95). Less acquisition
times could be achieved in the Warm Start case by
exploiting information acquired during the previous
start up.
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Channel 5
COMBINER
RECEIVER 1
RECEIVER 2
RECEIVER 3
Globalstar Handset
Globalstar Gateway
S1S1
S2 S2
Globalstar 1 Globalstar 2
Channel 5
Decoder
&
Vocoder
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Space SegmentDiversity Operation
Diversity operation provides significant advantages in both forward and reverse link transmission (combining is carried out by the user terminal and by the Gateway, respectively)
Spatial diversity in the forward link is illustrated: combining is performed on up to three received signal replicas
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Space Segment
Hard Handoff: Intrabeam Handoff (change of frequency)
Globalstar Handoffs Glo
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Ground Segment
GOCC: Ground Operations Control Center
SOCC: Space Operations Control Center
SPCC: Service Provider Control Center
Components
TT&C: Tracking, Telemetry and Command
GDN: Globalstar Data Network
GCC: Globalstar Control Center (incorporates GOCC, SOCC and GBO into a single facility)
GBO: Globalstar Business Office (for financial and administrative aspects:business arrangements with SP’s, billing, marketing and sales efforts
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Ground Segment
RFSUBSYSTEM
IS-41MSCVLR
BSC
CDMASUBSYSTEM
GSMMSCVLR
GATEWAY
GSM PLMN
HLR
GSMGMSCVLR
AInterface
PSTN
PSTN
PLMN
LOCALGSM MSC/VLR
Gateway - PLMN Interconnection
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User Segment
Main Characteristics:• GSM phase II/Globalstar Compliant• Voice/fax/data/SMS/SS GSM/GLB* Services• Position Location (up to 300 m)*• Automatic/manual Mode Select • Standard Battery 1600 mAh• Overall Weight 415 gr.• Overall Dimensions 21x6x4 cm• Stand-by and talk time in G* [2h - 7h]• Stand-by and talk time in GSM [4h - 83h*]• Graphic Display 4x12 characters + icons
Accessories:• Car Kit, Marine Kit, Home Kit• Data Terminal Adapter• Leather case• Cigarette Lighter Charger (12 Volt)• Desk Top Charger• Solar Charger
* if supported by the network
Globalstar User Terminals Status: Telit SAT 550 Glo
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Globalstar User Terminals Status: Telit SAT 650User Segment
Front shellController board
ShieldRadio board
Shield
Rear shell
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GS User-to-GS User Operation
In this case satellites in view offer, as usual, bent-pipe relays between users and relevant Gateways; whilst the Gateway-to-Gateway connection relies onto the PSTN backbone
Call Processing Glo
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Call Processing Simplified Call Procedure
A
User tries to place a call through the Globalstar Satellite service:
if the called party is a wireline or terrestrial cellular-based end user ( ), the call is routed through either the PSTN or PLMN
if the called party is a satellite-based end user ( ) the call is routed back through the Gateway up to the Globalstar Satellite and down to the user
Digital voice, low data rate applications [GSM, IS-54 (TDMA), IS-95 (CDMA), GLOBALSTAR, IRIDIUM…]
UMTS/IMT 2000 Global Standard for wireless multimedia
3G
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International Mobile Telecommunications-2000 (IMT-2000) are third generation mobile systems which are scheduled to start service around the year 2000 subject to market considerations. They will provide access, by means of one or more radio links, to a wide range of telecommunications services supported by the fixed telecommunication networks (e.g. PSTN/ISDN/IP), and to other services which are specific to mobile users
A range of mobile terminal types is encompassed, linking to terrestrial and/or satellite based networks, and the terminals may be designed for mobile or fixed use
As a strategic priority of ITU, IMT-2000 provides framework for worldwide wireless access by linking the diverse system of terrestrial and/or satellite based networks.
I M T - 2 0 0 0 T h e I T U v i s i o n o f g l o b a l w i r e l e s s a c c e s s
i n t h e 2 1 s t c e n t u r y
S a t e l l i t e
M a c r o c e l lM i c r o c e l l
U r b a nI n - B u i l d i n g
P i c o c e l l
G l o b a l
S u b u r b a n
B a s i c T e r m i n a lP D A T e r m i n a l
A u d i o / V i s u a l T e r m i n a l
IMT 2000
IMT is a result of the collaboration of many entities, inside the ITU (ITU-R Radiocommunication Sector and ITU-T Telecommunication Standardization Sector ), and outside the ITU (3GPP, 3GPP2, etc.)
3G
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3G
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Satellite Air interface selection - ITU Process
Satellite Wide Band CDMA (ESA RTT- Radio Transmission Technology). Adaptation of UMTS UTRA W-CDMA to the satellite environment. Suited for global systems (LEO/MEO). (SRI-A)
Formerly TTA- SAT.
(SRI-C)
(ESA RTT) Commonalities with ETSI UTRA TDD. Attractive for regional systems (HEO/GEO). (SRI-B)Harmonization
on going
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S-UMTS stands for the Satellite component of the Universal Mobile Telecommunication System. S-UMTS systems will complement the terrestrial UMTS (T-UMTS) and inter-work with other IMT-2000 family members through the UMTS core network. S-UMTS will be used to deliver 3rd generation mobile satellite services (MSS) utilizing either low (LEO) or medium (MEO) earth orbiting, or geostationary (GEO) satellite(s). S-UMTS systems are based on terrestrial 3GPP specifications and will support access to GSM/UMTS core networks.
Due to the differences between terrestrial and satellite channel characteristics, some modifications to the terrestrial UMTS (T-UMTS) standards are necessary. Some specifications are directly applicable, whereas others are applicable with modifications. Similarly, some T-UMTS specifications do not apply, whilst some S-UMTS specifications have no corresponding T-UMTS specification.
First set of ETSI Technical Specs approved (1/2) 3G
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First set of ETSI Technical Specs approved (2/2)
Satellite Component of UMTS/IMT 2000; A-family;
Part 1: Physical channels and mapping of transport channels into physical channels (S-UMTS-A 25.211)
Part 2: Multiplexing and channel coding (S-UMTS-A 25.212)
Part 3: Spreading and modulation (S-UMTS-A 25.213)
Part 4: Physical layer procedures (S-UMTS-A 25.214)
3G
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S-UMTS Air Interface transport and physical channels
The mapping of transport channels onto physical channels is a fundamental function performed by the physical layer
3G
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Worldwide Frequency Bands
ERC (European Radiocommunications Committee) assignments to MSS:
– 2 x 30 MHz (1980 - 2010 MHz and 2170 - 2200 MHz)– 15 MHz available from 2000 (1995 - 2010 MHz and 2185 - 2200 MHz)– 30 MHz available from 2005 (1980 - 2010 MHz and 2170 - 2200 MHz)– 15 MHz assigned TDMA systems (S-PCS) (1995 - 2010 MHz and 2185 -2200 MHz)
2X30 MHz in S-Band allocated to MSS, adjacent to spectrum allocation for terrestrial systems
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Spectrum Needs
More bandwidth requested
Terrestrial PCS are competing for spectrum allocation
WRC2000 (2000 World Radiocommunications Conference) postponed
a decision on satellite phone frequencies until 2003, which means that
before 2003 a viable satellite consortium needs to be established or else
the already allocated spectrum will be lost and available in favour of T-
UMTS
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From 3GPP 3G TS 22.105: UMTS Service aspects, Services and Service Capabilities
3G
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Again from 3GPP 3G TS 22.105 3G
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UMTS QoS Classes (1/2)
Differently from systems belonging to the previous generations, UMTS allows to enjoy the use of
bearers, defined by means of bearer service attributes, and not of end-services/applications directly.
To aid the application-to-bearer mapping, QoS classes for homogeneous end-services have been
devised, which are themselves service attributes, characterized by a set of specific service attributes,
as from the following viewgraph.
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UMTS QoS Classes (2/2)A
ttri
bu
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for
UM
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Bea
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Ser
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The “Satellite Access Network”
The access network infrastructure for the S-UMTS is here envisaged with minimal differences compared to the terrestrial 3G infrastructure. The satellite should play the role of the T-UMTS Node B (Base Station) but it’s to be deepened whether the same terrestrial Iur and Iub interfaces could be employed, which have been devised for T-UMTS between RNC’s and between RNC and Node B, respectively.
Iub ?
Iur ?
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S-UMTS Terminal : envisaged architecture
A digital predistortion in the TX path is envisaged, performed by the loop “DSP-Up conversion path-Antenna set-Feedback”. The same feedback line, shown in figure, is used to perform a dinamic adjustment, to improve the linearity of the receiving section.
The Control Processor manages the exchange of data/addressing information between the DSP and the ASIC
The core of the system is the DSP, responsible of most of the baseband processing; the support of dedicated ASICs for particular heavy computational operations like rake-decoding/Interference mitigation can be necessary depending on DSP computational power. In this last case, a dedicated bus between the DSP and the ASIC could also be needed, or the ASIC should directly communicate with the AD/DA converters and then with the DSP.