Optical communication as a driver for a data-centric ... · Optical communication as a driver for a...
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Optical communication as a driver for a data-centric
ground network service
SpaceOps Workshop 2013-06-11
Petrus Hyvönen, SSC, Sweden
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SSC as ground service provider
• SSC has been providing ground services to companies and agencies for 50 years
• Today a global network, PrioraNet is located at 10 sites with 34 operational antennas,
of which 14 are utilized as multi-mission
• PrioraNet is used by companies and agencies, including ESA, NASA, CNES, DLR,
CTLC, JAXA,…
• The PrioraNet network serves both polar and equatorial missions in Routine and
LEOP phases
• Today the service is RF based
• S-band for TT&C
• X-band for payload data acquisition
• Basic concept: Sharing of Resources between many missions
• Designed to maximize the use of ground resources
• EO pass is about 11 minutes each 90 minutes
• LEOP using the network during a limited time
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PrioraNet
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The TESLA optical link project
• SSC involved as a reference operator in
the RUAG-SZ led TESLA optical link
project
• Engineering Model Development ongoing
for space terminal and optical ground
station
• Flight model ready in 2016
• 1550 nm laser, on-off keying gives robust
link
• Space Terminal for small LEO satellites
• 5 kg mass
• 45 W power consumption during downlink
• 2 Gbps user downlink data rate
• Ground Terminal Prototype
• 0.6 m diameter telescope
• Bidirectional asymmetrical link needed for
link signaling but can also upload
commands
• Minimum elevation 20 deg above horizon
for prototype
TESLA Ground station protype at RUAG-SZ
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From prototype to operational
Left: „Double Tube“ Right: „Fork Mount“, dual instrument
• Future system upgrades achieved by adding secondary (telescope) payload to same mount
• Today 80 cm telescopes available at similar price as 60 cm prototype telescope
• 80 cm telescope allows lower elevation angle down to 15 degrees (about 1.5x longer downlink time)
OB + Elec 1 OB + Elec. 2
OB + Elec 2
OB + Elec 1
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Baseline Scenario for discussion
• Earth Observation satellites in
Sun Synchronous orbit (polar
orbit)
• Onboard memory for data
storage
• Optical communication for high
data rate payload downlink
• Limited but existing uplink
capabilities on optical link, such
as the TESLA link
• RF for TT&C, Emergency and
LEOP
• Optical ground network of
several stations, serving several
users
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General overview of operational concept in RF
• Service Level Agreement defined in contract with satellite owner / operator
• Rough planning of supported passes 1-2 weeks ahead
• Detailed schedule and pass confirmations made 2 days ahead
• For payload data, spacecraft is often pre-programmed to start data
transmission by time tagged commands
• Very high pass success rate on RF, outages are mainly technical failures,
environmental factors hardly influence successful pass rate
The process is mature, very well defined, and repeated literally hundreds of
times per day. The downside is that it is not easily changed.
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Main operational Difference optical – current RF
• Sensitivity to Weather
• No / Part / Full communications
during pass
• Communications intermittent
during pass
• Higher elevation than RF needed
• 15-25 deg compared with 5 deg
for RF
• Local weather, season, can strongly
influence link probability
These factors have profound effects on
the needed operational principles..
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Historical Cloud Coverage Analysis results in a
distribution of daily contact durations
• Clear sky availability analysis
performed in TESLA project by GMV,
SA, Spain, based on CDFS-II cloud
data base
• Statistical evaluation of clear sky
conditions at 7 selected sites including
PrioraNet sites for the years 2002-
2010
• Reference parameters • 700km SSO
• Min elevation 25 deg
• Solar exclusion angle +-10 deg
• Histogram shape allows Gaussian Fit
for network; fits well to Binomial
distribution model ~33% cloud
probability per single site 10 20 30 40 50 60 70 80 90
0
0.005
0.01
0.015
0.02
0.025
0.03
0.035
0.04
[min] contact per day
De
ns
ity
7 sites PDF and Gaussian fit, =44.3841 sig=11.1482
7 sites data
Gauss fit
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PrioraNet Station Cloud Statistics
Esrange, Northern
Sweden
Santiago de Chile Western Australia
Space Center
Altitude 341 m 520 m 34 m
Day Mean Cloud
Coverage
59%
34%
34%
Night Mean Cloud
Coverage
55% 33% 28%
Max Contact Minutes
per day*
25.5 min
10.8 min
11.2 min
Mean Contact
Minutes per day incl.
Cloud coverage*
9.9 min
6.2 min
6.3 min
Mean Tbit/day* 1.2 0.9 1.0
*System estimates with a 700 km SSO, TESLA prototype performance OGS (60 cm telescope, 25 deg min
elevation).
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How to operate within this limitation
• Forget passes
• Forget predicted scheduling
• Focus on data delivered not individual stations
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Passes
• The concept of operations by passes as the
main quantifier needs to go away • Pass can be Completely cloudy
• A pass can be partly cloudy
• Full pass
• No blind downlinks by time tagged commands,
all data downloads must be triggered
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Ground Network Metrics
• Data Capacity (TB / day)
• Optical strength
• Latency (minutes or hours)
• RF strength due to robust reception
• Can be partly overcome by using
priority on data level
• Direct coverage (Area)
• Coverage area depending on
elevation angle
• RF has larger coverage than optical
• Optical higher bitrate
Latency map for RF network
Capacity:
Punta Arenas 4.67 Pass/day
Esrange 9.50 Pass/day
Inuvik 9.67 Pass/day
WASC 3.00 Pass/day
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Service Level Agreement for Optical
630 km SSO, 7x 80cm OGS, 2x 1Gbit/s downlink, 33% cloud probability per site
6 Tbit/24 hrs at 95% probability
This would be the starting point for a SLA for a optical ground service.
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0.00
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7654321
Pro
bab
ilit
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Tb
it p
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day
Sites with clear sky
Tb per 24 hours Probability of clear sky
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Focus on Data
• Focus on the data as
files / group of
packets
• Provide a service
based on priority of
data, can differ on
single mission and/or
between missions
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Scheduling of Optical Ground Stations
• Constant scheduling needed
(including what we today call
’rescheduling’)
• Knowledge at Network Management
Center (NMC) of current weather systems
and forecasts at the ground stations
• Flexible and adaptable priority scheme in
order to deliver latency sensitive data first
• Scheduling rules need to be established
based on some TBD data quantifier, file /
group of packets to ensure lowest latency
of usable products
• Ground network capabilities part of
scheduling algorithm
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Data handling & Dissemination
RF System
• Bent pipe data to customer
• For high data rates data is
temporarily stored at the receiving
ground station
• Pass based quantification of data /
file
• High bitrate communications from
ground station to customer
Optical System
• RF architecture based on pass will
not work
• Fragments of data spread among
different stations
• Received data is assembled from
multiple locations to produce a
deliverable product
• Data distribution either through
central repository or in bittorrent-
type
• Large datasets – don’t transfer
data you don’t need
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Satellite Impacts
RF System
• Satellite owner performs all
commanding, ground network
as bent-pipe
• Often time tagged commands
for data dumps
• Distinct separation of customer
/ ground network
Optical System
• Owner performs satellite
tasking, ground network
schedules its resources
• Satellite owner prioritizes
which data to downlink
• Ground network signals to
satellite when a resource is
available for downlink
• Onboard memory sized for
acceptable service level
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Service Formulation
• The service formulation should be clear to the satellite owners in order to
design the on-board memory accordingly
• The ground network provider needs clearly set requirements on how to
operate the system in terms of allocating ground resources to the different
satellite users.
• Detailed simulations are needed to find the quantitative expression but a
starting point should be that the system delivers for example 12 Tb of data
to a certain network location, over 48 hours, with a probability of 95%.
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What about upcoming RF
• High bitrates also coming for Ka-,
K-band (26 GHz) LEO
• K-band (from ESA EUCLID info):
• Full loss (with any stronger rain,
possibly with any rain, depending
on the link margin), expected for
1% to 2% of the time.
• Intermediate/scintillation range
with cut off of the scintillation
frequency at ~10 Hz. (i.e. link
conditions can be assumed as
constant over 0.1 s).
• Good range (here the K-band link
works as well as any other radio
link), expected for 90% of the
time.
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Ka-band properties
• Ka band usage in LEO is different from high elevation GEO applications
• LEO tests with the Australian FedSat mission (20 GHz)
• Atmospheric channel distortions at low elevation angles are pronounced in
Ka band, requiring higher elevation angles (>10° ?) • significant increase in high-frequency fading
• terrestrial multipathing limits the spectral efficiency
• Weather dependency
From: ”Ka Band Propagation Experiments on the Australian Low Earth Orbit
Microsatellite ‘FedSat’”
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Optical as a driver for next generation
ground network service?
• The characteristics of weather dependency is not only
for optical – also higher RF frequencies
• The current S- and X-band operational pass based
concept might not be suitable for high frequency RF or
optical
• Although less sensitive than optical, the proposed
service type would be suitable for RF and potentially
advantageous
• Optical can be a driver of this transformation with the
necessity of new operative concepts, new protocols,
and architectures
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Questions
• New operational concepts, but one operative system
that supports both optical and future RF: • Division of functionality between network provider and satellite operator?
• Service Management Interfaces?
• Service Delivery Interfaces?
• How do we design these interfaces and what protocols
are needed / selected? (DTN, CFDP, Bittorrent…)
• How do we ensure that the two segments space and
ground are designed and optimized as one system? • Downlink requirements
• Onboard storage
• Near reception processing
• …