Gaia status
Anthony Brown
Sterrewacht Leiden, Leiden University brown@strw.leidenuniv.nl
Place - Date - 1/43
Gaia status Anthony Brown Sterrewacht Leiden, Leiden University - - PowerPoint PPT Presentation
Gaia status Anthony Brown Sterrewacht Leiden, Leiden University brown@strw.leidenuniv.nl Place - Date - 1/43 Gaia summary Gaia: science with 1 billion objects in three dimensions ESA corner stone mission building on the Hipparcos
Anthony Brown
Sterrewacht Leiden, Leiden University brown@strw.leidenuniv.nl
Place - Date - 1/43
three dimensions
Spectroscopy
management and operations by ESA, and data processing by scientists (DPAC)
Soyuz from Kourou
18 July 2014
summer 2016, but Science Alerts start earlier
w w w . c
m
. e s a . i n t / g a i a
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Astrometric Field CCDs Blue Photometer CCDs Sky Mapper CCDs 104.26cm 42.35cm Red Photometer CCDs Radial Velocity Spectrometer CCDs Image motion
Basic Angle Monitor Wave Front Sensor Basic Angle Monitor Wave Front Sensor
Figure courtesy Alex Short Total field:
Sky mappers
Astrometry
Photometry
Spectroscopy
Place - Date - 6/43
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January 2014
14 January
started on 8 January
July 18 2014
Sky coverage Feb 7 to May 24 IDT team @ University of Barcelona
Detailed report: GAIA-CO-TN-LEI-AB-052
Place - Date - 10/43
NGC 2516 Gaia DSS
Place - Date - 11/43
M51
Place - Date - 12/43
Diagrams courtesy C. Jordi and J.-M. Carrasco
Place - Date - 13/43
Diagrams courtesy C. Jordi and J.-M. Carrasco
Place - Date - 14/43
Figure courtesy D. Katz,
Place - Date - 15/43
840 850 860 870 880 2000 4000 6000 8000 10000 Flux (photoelectron/sample)
Calibrated spectra on the 3 AL RVS CCD for a K-type star
internalApparentGrvs = 5.50 840 850 860 870 880 2000 4000 6000 8000 10000
Flux (Photoelectron/sample) 840 850 860 870 880 Wavelength (nm) 2000 4000 6000 8000 10000 Flux (Photoelectron/sample)
strip 1 strip 2 strip 3
RV(dir) = -68.89 +- 3.17 RV(fou) = -69.30 +- 1.87 RV(mdm) = -68.68 +- 0.07 Spectroscopic Radial Velocity = -68.89 +- 3.17 km/s
Early result from automated RVS processing
Credits: ESA/Gaia/DPAC/CNES/Yves Viala and Francoise Crifo
Place - Date - 16/43
◮ plenty of propellant left for future manoeuvres
◮ Chemical propulsion system for large manoeuvres ◮ Micro propulsion system to maintain Gaia’s spin rate and compensate solar radiation pressure torque ◮ Attitude and Orbit Control System works will within specs; thermal control fine ◮ Good link budget for phased array antenna → high data rates possible
◮ Validation of high accuracy time correlation pending
◮ 106 CCDs and 106 back-end electronics units all working fine ◮ 7 on board computers managing the CCDs and electronics ◮ Payload and data handling unit for storing and down-linking data ◮ Telescopes aligned and focused; good image quality over full FPA
◮ Excellent flight control team at ESOC ◮ DPAC operations teams calm and competent ◮ About 40 DPAC Payload Experts analyzed the data; supported commissioning ◮ Many S/W patches and fixes but all in controlled manner
Place - Date - 17/43
Gaia seen by ESO-VST: image courtesy ESO
Place - Date - 18/43
Background
and 2.5 mm/s in each velocity axis (aberration correction bright stars)
◮ 1 mm/sec upper limit on systematic error!
◮ Can only be achieved after first AGIS solution
Status
◮ VST@ESO can deliver the required astrometric precision most of the time and is now the backbone of GBOT ◮ Observing/processing strategy being adapted at Liverpool Telescope, which should deliver the required astrometric precision ◮ Test observations underway with Las Cumbres 2m telescopes
Place - Date - 19/43
propulsion system
◮ Erroneous feedback from this thruster to the Attitude and Orbit Control System, leading to increased gas consumption, and possibly degraded attitude control
◮ AOCS works very well ◮ Slight cold gas over-consumption due to thruster bias drifts ◮ Bias being monitored and calibrated ◮ Studies ongoing to optimize MPS usage
◮ lost redundancy for this CPS thruster ◮ New CPS mode implemented which makes Gaia robust against thruster 3A failure
Place - Date - 20/43
magnitude above requirements
scattered at sun-shield edges
◮ Varies over 6 hour spin period
along unforeseen paths
◮ Varies according to sky scanned
SAA= 45◦ SAA= 0◦ Figures by M. Davidson Sun dominates Night sky dominates time → Flux [e−/pix/s]
Place - Date - 21/43
0.0 0.1 0.2 0.3 Response loss [mag] 260 380 500 620 740 860 980 1100 1220 1340 1460 OBMT [rev] FoV 1 FoV 2 SP6 SP1 Figure by C. Fabricius
Decon 1 (FOV2) Decon 2 Decon 3 Decon 4
Monitoring of response by comparison to Tycho-2 photometry
Place - Date - 22/43
Figure by FL Scientist team
Place - Date - 23/43
0.0 0.02 1320 1340 1360 1380 1400 1420 1440 1460
FFF,Fovf∆Grevτ
OBMT [rev] AF FoV1 BP FoV1 RP FoV1 AF FoV2 BP FoV2 RP FoV2
Figure by FL Scientist team
◮ Not clear at the moment how many more
PE analyses ◆ Modelling effects of ice
◮ XP spectral signatures ◮ image quality
◆ Optimization of the decontamination procedure
◮ heating all mirrors seems necessary
Place - Date - 24/43
∆(δγ) [mas]
500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000
no of 5-minute-interval
791.007 799.007 807.007 815.007 823.007 831.007 839.007 847.007 855.007 863.007 871.007 879.007 887.007
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 white-light fringe experiment slew to NSL
→ Time [spin period] → BA variation [mas] Figure by First Look team BA variation according to BAM BA variation according to ODAS
◮ 6 hour variations can cause systematic errors in astrometry ◮ Basic Angle Monitor (BAM) in place to measure the variations so they can be accounted for in processing
Place - Date - 25/43
Including: BR CA DZ ESA IL US DPAC participating countries October 2013 450 members DPCI DPCG DPCC DPCB DPCT DPCE
Pan-European cooperation
◮ Academic institutions and national space agencies ◮ Supported through national funding ◮ Processing power spread
◮ SOC/DPCE integral part
CU3 Initial Data Treatment First Look ESAC CU3 Astrometric core processing ESAC/Torino CU5 Photometric processing Cambridge CU6 Spectroscopic processing CNES MDB ESAC CU3 Intermediate Data Update Barcelona CU7 Variability analysis Geneva/ISDC CU4 Complex object processing CNES CU8 Astrophysical characterization CNES Telemetry ESOC CU1 System/IT architecture CU2 Simulations Barcelona/CNES CU9 Archive and Catalogue access ESAC Alerts Transients, new SSOs, . . . Cambridge/CNES
Upstream Downstream
Place - Date - 27/43
Example TM time line with Galactic plane crossings (OBMT rev 516–517, courtesy J. Hern´ andez)
Place - Date - 28/43
Statistics up to October 10 Data collected or processed Type of Data Amount Science telemetry 7.6 TB Astrometry transits 9.0 × 109 90 × 109 images Photometry transits 8.8 × 109 17.6 × 109 images Spectroscopy transits 1 × 109 3 × 109 spectra
Place - Date - 29/43
20000 40000 60000 80000 100000 120000 50000 100000 150000 200000 250000 300000 350000
1 2 3 4
1 2 3 4
frequency primary sources, FoV1, WC1 frequency ǫη [mas] secondary sources, FoV1, WC1 primary sources, FoV2, WC1 ǫη [mas] secondary sources, FoV2, WC1
solution at G = 15 already better than 1 mas
◮ unstable instrument ◮ poor PSF calibrations ◮ imperfect stray light corrections ◮ throughput loss
expected
under control
nominally (detailed verification pending)
Figure courtesy First Look team
Place - Date - 30/43
classification and parametrization possible
is as expected
non-uniformity under control
Figure courtesy C. Jordi & J.-M. Carrasco
Place - Date - 31/43
Figure courtesy D. Katz &
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Figure by CU6 Payload Experts
ground based radial velocity standards
Place - Date - 33/43
measured against dedicated Ecliptic Pole survey
G < 6 through detection algorithm improvements and employment of special
Figures courtesy U. Bastian and SOC Calibration Team
Place - Date - 34/43
Credits: M. Fraser/ S. Hodgkin/ Ł. Wyrzykowski/
SDSS Place - Date - 35/43
Performance predictions for G2V star V magnitude Astrometry Photometry Spectroscopy (parallax) (BP/RP integrated) (radial velocity) 3 to 12 5–14 µas 4 mmag 3 to 12.3 1 km s−1 15 24 µas 4 mmag 15.2 15 km s−1 20 540 µas 60 (RP) – 80 (BP) mmag Up-to-date information always at: http://www.cosmos.esa.int/web/gaia/science-performance
Place - Date - 36/43
◮ Systematics not accounted for
accounted for perfectly, the current numbers provide an optimistic performance estimate
◮ Basic Angle variations ◮ Throughput loss (with corresponding optical quality degradation) ◮ Micro-meteoroid hits ◮ Radiation damage
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Impacts on data processing
◮ Later start of nominal operations and processing
◮ Effect of future decontamination campaigns ◮ Stray light effects ◮ Change in RVS observing strategy ◮ Account for basic angle variations through BAM measurements ◮ Deal with high rate of micro-meteoroid hits ◮ More complex data validation
Place - Date - 39/43
◮
◆ Gaia now routinely observes all sources 3 ≤ G ≤ 21
◮
◆ Data collected: 150 GB HKTM, > 6.5 TB science data
◮ Operational data base 62 TB
Place - Date - 40/43
Basic angle related Working group will look into root cause of BA variations (Airbus DS, ESA, DPAC). Research and development on calibrating the BA variations using a combination of AGIS adaptations and BAM measurements − → will take time! Contamination Optimize strategy to deal with future decontamination campaigns (with Airbus DS support): procedure when to do decontamination, thermal conditions, recovery time Stray light related Support from Airbus DS to develop and implement an
changes to be managed by Airbus).
Place - Date - 41/43
DPAC Payload Experts at institutes throughout Europe Initial Data Treatment, First Look, and AVU/BAM+AIM teams Operations teams at ESAC, Torino, CNES-Toulouse, Cambridge, Barcelona, Geneva ESA Gaia-SOC calibration team DPAC Project Office ESA Gaia Project Scientist team ESOC flight control team ESA Gaia project team Airbus Defence & Space Arianespace, Soyuz, CNES-Kourou launch teams
Place - Date - 42/43