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www.elsevier.com/locate/asr
Advances in Space Research 37 (2006) 1710–1715
ALTEA data handling
L. Di Fino a, F. Belli a, V. Bidoli a, M. Casolino a, L. Narici a,*, P. Picozza a, A. Rinaldi a,D. Ruggieri a, V. Zaconte a, S. Carozzo b, W.G. Sannita b,c, P. Spillantini d, V. Cotronei e,
E. Alippi f, G. Gianelli f, A. Galper f, M. Korotkov g, A. Popov g, V.P. Petrov h,V.P. Salnitskii h, S. Avdeev i, W. Bonvicini j, G. Zampa j, N. Zampa j, R. Vittori k,
C. Fuglesang l, D. Schardt m
a INFN and University of Rome Tor Vergata, Department of Physics, Via della Ricerca Scientifica 1, 00133 Rome, Italyb Neurophysiopathology-DISM, University of Genoa, Genoa, Italy
c Department of Psychiatry, SUNY, Stoony Brook, NY, USAd Department of Physics, University and INFN, Florence, Italy
e Italian Space Agency, Rome, Italyf Alenia Spazio S.p.A. – Laben, Milan, Italy
g Moscow State Engineering Physics Institute, Moscowh Institute for BioMedical Problems, Moscow, Russia
i Cosmonaut, Russian Space Corporation �Energia� by name Korolev, Korolev, Moscow region, Russiaj Department of Physics, University and INFN, Trieste, Italy
k ESA Astronaut and INFN, Perugia, Italyl ESA Astronaut, Royal Institute of Technology, Stockholm, Sweden
m GSI/Biophysik, Darmstadt, Germany
Received 14 October 2004; received in revised form 21 January 2005; accepted 31 January 2005
Abstract
The ALTEA program is an international and multi-disciplinary collaboration aimed at studying particle radiation in space envi-
ronment and its effects on astronauts, in particular the anomalous perception of Light Flashes. This paper describes ALTEA space
facility scheduled to fly in the International Space Station (ISS) after July 2006, what kind of data are produced and how data are
transmitted to Earth, processed and analyzed.
� 2006 Published by Elsevier Ltd on behalf of COSPAR.
Keywords: ALTEA; Cosmic rays; Data handling; ISS; Light flash
0273-1177/$30 � 2006 Published by Elsevier Ltd on behalf of COSPAR.
doi:10.1016/j.asr.2005.01.105
Abbreviations: ALTEA, Anomalous Long Term Effects on Astronauts; ASI, Italian Space Agency; ASMP, Asymmetric MultiProcessor; BEU,
Brain Explorer Unit; BNL, Brookhaven National Laboratory, Upton, NY, USA; CNSM, Central Nervous System Monitoring; DAU, Data
Acquistion Unit; DOMSAT, Domestic Satellite; DOSI, Dosimetry; DSP, Digital Signal Processing; EEG, ElectroEncephaloGraph; GSI, Institute
for Heavy Ion Research, Darmstadt, Germany; HIT, Heavy Ion Therapy; ISS, International Space Station; LET, Linear Energy Transfer; LOR,
Line Outage Recorder; LTU, LapTop Unit; MARS, Microgravity Advanced Research and Support; MICE, Mice Irradiation with Concurrent
Electrophysiological monitoring; MIP, Minimum Ionizing Particle; MSFC, Marshall Space Flight Center; OBT, On Board Time; PBU, Push Button
Unit; POIC, Payload Operations Integration Center; RIC, Rack Interface Controller; SDS, Silicon Detector System; SDU, Silicon Detector Unit;
SGS, Space-to-Ground Subsystem; SSCC, Space Station Control Center; TDRSS, Tracking and Data Relay Satellite System; UHB, User Home
Base; USOC, User Support and Operation Center; VSU, Visual Stimulator Unit; WSC, White Sands Center.* Corresponding author. Tel.: +39 0672594519; fax: +39 062023507.
E-mail address: [email protected] (L. Narici).
L.D. Fino et al. / Advances in Space Research 37 (2006) 1710–1715 1711
1. Introduction
The length of manned space flights (operations in the
International Space Station (ISS) or the planned journey
to Mars) will significantly increase in the near future.
Anomalous Long Term Effects on Astronauts (ALTEA)is an international and multi-disciplinary program
aimed at studying the effects of particle radiation on
the Central Nervous System during long manned mis-
sions on board ISS, in particular the anomalous percep-
tion of Light Flashes (Casolino et al., 2003). ALTEA
includes a space facility scheduled to fly and operate in
the ISS after July 2006 (Narici et al., 2003).
This paper describes what kind of data are producedby this facility and how data are transmitted to Earth,
processed and analyzed; it consists of five main sections.
In the first section a quick overview of the apparatus and
its main scientific objectives are presented. The second
section deals with different experiment configurations
and data produced during ALTEA space experiments.
Third section is about audio and video requirements.
Fourth section describes in details data path duringtransmission from ISS to ALTEA User Home Base
(UHB) in University of Rome Tor Vergata. Last section
gives a hint about processing and analysis of ALTEA
scientific data.
Fig. 1. Schematic view of ALTEA facility: it is possible to see all
ALTEA devices attached to Express Rack during CNSM mode;
technical specifications are given for each component. In the upper left
corner a 3D view of ALTEA inside ISS.
2. ALTEA facility: general description
ALTEA is a multi approach program. It consists of
various experiments both laboratory based and onboard
ISS. Ground experiments are:
� ALTEA-MICE (Sannita et al., 2004): started in 2001
at GSI and BNL
� ALTEA-HIT: started in 2004 at GSI
� ALTEA-Biophys: started in 2003 at GSI
Space experiments are:
� Alteino (Casolino et al., 2002): onboard ISS since
April 2002
� ALTEA Light Flash Questionnaire (Fuglesang et al.,
2004): started in 2003
� ALTEA-Space: scheduled to fly in December 2005� Other future uses of the ALTEA Facility (ALTEA-
3D, ALTEA-Shield, etc.)
ALTEA-Space will measure on board ISS the parti-
cles passing through the brain of the astronauts and
monitor the cortical electrophysiological activity and
the visual system functional status. The goal is to define
and measure electrophysiological descriptors of brainfunctioning and to correlate their dynamics with space
environments (Narici et al., 2004). Measures of re-
sponses to proper visual stimuli will permit to assess
the visual system status. It will also operate in un-
manned mode to allow long term measurement of parti-
cle fluxes inside the ISS.
The ALTEA facility (see Fig. 1) is composed by:
� Data Acquisition Unit (DAU)
� Silicon Detector System (SDS) – composed by 6 par-
ticle detectors (SDU)
� Brain Explorer Unit (BEU) – 32-channel ElectroEn-
cephaloGraph (EEG)
� Visual Stimulation Unit (VSU)
� Push Button Unit (PBU)
� LapTop Unit (LTU)
The Data Acquisition Unit (DAU) is connected with
the 6 Silicon Detector Units (SDU) and with the Visual
Stimulation Unit (VSU). The DAU and the LapTop
Unit (LTU) are connected via TCP/IP with the ISS
using the Rack Interface Controller (RIC) connections.
ALTEA is an autonomous experiment from the point of
view of the interaction with Ground: no remote controlis foreseen and just an initial and guided participation of
the astronaut to experiment set-up is required. All data
from ALTEA are in the form of Express Rack Teleme-
Table 1
Structure of an Express Rack Telemetry packet
Table 2
Telemetry data: main data types are reported together with packet size
and frequency of acquisition
Telemetry data type Packet size
(bytes)
Frequency of
acquisition
Science SDS data 122–1266 Event driven
Service data 24 Event driven
Nominal housekeeping 232 10 Hz
EEG data 1074 1024 Hz
Health & status 34 1 Hz
1712 L.D. Fino et al. / Advances in Space Research 37 (2006) 1710–1715
try packets. In Table 1 the structure of a telemetry pack-
et is described. In Table 2 various kinds of telemetry
data are reported together with packet length and
frequency of acquisition. Scientific telemetry data and
service data generation depend on instrument
operating mode and on involved subsystems. SDS gen-
erates periodic scientific data only in calibration mode,
otherwise data generation is triggered by particledetection.
3. Experiment configurations and expected data rates
The two main ALTEA-Space configurations are
named Dosimetry (DOSI) mode and Central Nervous
System Monitoring (CNSM) mode and they are, respec-tively, unmanned and manned operative modes. AL-
TEA will continuously operate in DOSI mode for a
period of one increment without human intervention.
There will be six interruptions corresponding to the
CNSM sessions. During DOSI mode ALTEA measures
radiation fluxes on board ISS. Only Silicon Detector
System (SDS) is switched on and data are downloaded
in real-time, without any local storage. Expected datarate is about 0.65 Mbps, so the estimated storage size
for the whole increment is about 1.3 Tb. Second opera-
tive mode is CNSM. Six 90-min sessions are planned as
follows: an astronaut will wear the EEG cap, insert his/
her head in the SDS and will signal perceptions of Light
Flashes with a pushbutton while SDS will measure cos-
mic rays flux through his head, so that it will be possibleto study concurrently the passage of cosmic radiation
through the brain, the functional status of the visual sys-
tem and the electrophysiological dynamics of the corti-
cal activity. Data are stored on the ISS laptop.
Expected data rate is 1.4 Mbps and each session is ex-
pected to take up about 1.5 Gb. Data are then down-
loaded off-line and erased from the laptop only after
positive transmission check.
4. Audio and video
To assure optimal setup of the experiment, real-time
audio and video communications are required. The
audio will be a bidirectional system, while video will
be a one-way system from ISS to earth. Fig. 2 shows aschematic view of experiment timeline in which audio
and video communications are reported: we asked
for recorded video during the entire system setup
and during CNSM setup, while realtime video and
audio will be used only in the last 10 min of system
setup and the first 15 min of CNSM setup. A second
astronaut will help the subject during part of the CNSM
sessions.
5. ALTEA data flow
This section deals with transmission of data from the
Payload on board ISS to the ALTEA UHB, where data
are stored and analyzed. Composition of Space Segment
and Ground Segment are described together with Trans-mission Bands used for communications and data distri-
bution between different segments. In Fig. 3 there is a
block view of the entire data flow.
5.1. Space data segment
5.1.1. Onboard ISS
ALTEA is installed in an Express Rack, that providesstandard and simple interfaces to payloads, and it com-
municates over a local LAN to the RIC. The RIC is con-
figured as a passive server and provides the
communication link between payloads and the Space
Station data system and ground controllers. The RIC
will route the payload data in packets (Express Rack
Packets), with headers to identify the payload (see Table
1), and it will transmit them through the Space Stationdata system. All communications onboard ISS are based
on TCP protocol.
Fig. 3. Schematic view of ALTEA data flow: data are produced by ALTEA facility on board ISS (Section 5.1.1), then transmitted through TDRSS
and WSC (Section 5.1.2) to NASA Ground Segment (Section 5.2.1) and finally to Italian Ground Segment (Section 5.2.2).
Fig. 2. Schematic view of ALTEA experiment timeline: it is possible to see recorded video during the entire system setup and realtime video and
audio communications during part of the setup.
L.D. Fino et al. / Advances in Space Research 37 (2006) 1710–1715 1713
5.1.2. TDRSS and WSC
All ISS communications to Earth are vehiculated by
Tracking and Data Relay Satellite System (TDRSS).TDRSS consists of 6 satellites in geosynchronous orbits
and a dedicated ground station. The main task of the
TDRSS is to provide communication and tracking ser-
vices for ISS and other low-earth orbit spacecrafts.
TDRSS operates as a repeater, relaying signals to and
from the ground station. No data processing is done on-
board the TDRSS.
The ground station that monitors and controls thesatellites is the White Sands Ground Terminal in New
Mexico. White Sands Center (WSC) has a Line Outage
Recorder (LOR) that records data in case a connection
between WSC and one of the NASA centers fails. If thathappens, WSC can play back the data when the connec-
tion is restored.
5.1.3. Data transmission bands
Transmission Bands used for communications and
data distribution between Space Segment and Ground
Segment are S-band and Ku-Band.
S-band data is relayed to/from ISS via TDRSS.S-Band carries primarily core system data down and
1714 L.D. Fino et al. / Advances in Space Research 37 (2006) 1710–1715
commands up. S-Band operates at 2065.0 and
2085.6875 MHz and it is used for the forward and return
link to ISS.
Ku-Band is used as a return data link and data is sent
from the ISS Space-to-Ground Subsystem (SGS) to
White Sands via TDRSS. Data are then sent to thecontrol centers, and finally to remote users. Ku-Band
operates at 13,775 and 15003.4 MHz and primarily
carries High Rate Payload Data, Digital Video (video
is converted from analog to digital onboard and sent
down as a part of the Ku-Band data) and Core Playback
Data.
5.2. Ground data segment
5.2.1. NASA ground segment
The two main nodes of NASA Ground Segment are
Space Station Control Center (SSCC) at Johnson Space
Center and Payload Operations Integration Center
(POIC) at Marshall Space Flight Center (MSFC).
Planning and procedure data are exchanged between
SSCC, POIC and the Italian Ground Segment. Audiocoordination is used between sites on the ground. The
POIC is responsible for scheduling, managing, and con-
trolling the Space Station onboard payload data and
video systems. ALTEA data is received at MSFC�sPOIC that has the overall responsibility for payload
ground data distribution. At MSFC there is also the
capability to monitor vital payload information. Beside
ALTEA scientific data, other kind of data will be dis-tributed: ISS System Telemetry, Air-to-ground Audio
and Air-to-ground Video. Data are distributed to
remote sites using UDP protocol.
Fig. 4. Schematic view of ALTEA UHB: it is possible to see the structure of
the storage server and the devices for communications and data presentatio
5.2.2. Italian ground segment
Data are transmitted to Italian Segment from the
Italian Space Agency (ASI) Gateway (USA) through
the ASI-Net backbone to the Microgravity Advanced
Research and Support (MARS) Center in Naples that
operates as ASI Italian User Support and OperationCenter (USOC) and that is responsible for the opera-
tions of the Italian Payloads onboard ISS. Finally data
reach ALTEA UHB.
5.2.3. ALTEA UHB
ALTEA UHB will be able to monitor experiment, to
store and to analyze collected data. UHB configuration
will be the following (see Fig. 4):
(1) One Data Storage Server (with redundant disk
array).
(2) One or more multi-processor workstation for
Scientific Data Analysis.
(3) One Video-Conference workstation for video-con-
ference communications with NASA.
(4) One Voice-Loop workstation for audio-communi-cations with ISS.
(5) One wide screen monitor/video projector to
display ISS real-time video or scientific data.
We are considering the use of multi-processor Linux
workstations with specially developed Asymmetric Mul-
tiProcessor (ASMP) real-time kernel and dedicated Dig-
ital Signal processing (DSP) boards for real-timeanalysis. ASMP kernel allows to entirely dedicate one
or more processor to specific tasks, reducing overhead
due to standard system operations.
the User Home Base with the private LAN, the analysis workstations,
n.
L.D. Fino et al. / Advances in Space Research 37 (2006) 1710–1715 1715
6. ALTEA data analysis
6.1. DOSI analysis
In DOSI mode Health & Status and Housekeeping
data such as voltages, currents and temperatures willbe monitored to ensure proper functioning of all the
instrumentation and to allow emergency deactivation
or to shut down any system or subsystem. Off-line anal-
ysis of scientific data will be able to process scientific data
relative to SDS subsystem, performing pedestal subtrac-
tion, adaptive pedestal correction, bad data rejection,
particle track reconstruction, released energy calcula-
tion, Linear Energy Transfer (LET) calculation, nuclearspecies discrimination, relative and absolute nuclear
abundances calculation, differential and integral radia-
tion fluxes calculation and statistics on particle direction.
In addition to this some ancillary data of the ISS (posi-
tion, altitude and inclination) will be correlated with
ALTEA data to obtain information about radiation
fluxes in different geomagnetic zones. Work is in progress
to process a subset of these operations in real-time, in or-der to issue space radiation warnings to the crew.
6.2. CNSM analysis
In CNSM mode, all subsystems will be switched on,
and in addition to previous ones there will be data from
EEG and Push Button Unit (PBU). CNSM data will be
analyzed off-line to measure the energies and trajectoriesof the cosmic particles passing through the astronaut�s
brain concurrently with his brain electrophysiological
dynamics. Particle trajectory and absorbed doses in
brain will be calculated and the correlation between
the energy released in different cortical regions and
changes in the electrophysiological signal will be stud-
ied. This will allow to define new risk parameters linkedto the interaction in space between ion passages and
brain functions.
Acknowledgement
ALTEA is funded by the Italian Space Agency.
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