status of telescope fabra roa montsec (tfrm)lfvn.astronomer.ru/report/0000078/tfrm_rev4.pdf ·...
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![Page 1: Status of Telescope Fabra ROA Montsec (TFRM)lfvn.astronomer.ru/report/0000078/tfrm_rev4.pdf · 2011-09-25 · Primary mirror 0.78mPrimary mirror 0.78m CCD FoV 4.41deg x 4.41degCCD](https://reader034.vdocuments.pub/reader034/viewer/2022042712/5f90e37ebbea615cf1740331/html5/thumbnails/1.jpg)
Fors O.Fors O.1,21,2, Montojo F.J., Montojo F.J.33,, NNúñúñez J.ez J.1,21,2, Mui, Muiñños os
J.L.J.L.33, Boloix, J., Boloix, J.3,3, Baena R.Baena R.1,21,2, Morcillo R., Morcillo R.33, ,
Merino M.Merino M.1,21,2
(1): Observatori Fabra, Reial Acadèmia de Ciències i Arts de Barcelona
(2): Dept. d’Astronomia i Meteorologia and Institut de Ciències del Cosmos
(ICC), Universitat de Barcelona (UB/IEEC)
(3): Real Instituto y Observatorio de la Armada (ROA)
Status of Telescope Status of Telescope
Fabra ROA Montsec (TFRM)Fabra ROA Montsec (TFRM)
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
Optical Observations for Space Surveillance & TrackingOptical Observations for Space Surveillance & Tracking
Contact: [email protected]@am.ub.es
Further info: http:http://www.am.ub.es/bnc//www.am.ub.es/bnc
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OverviewOverview
AMOS 2011, 13AMOS 2011, 13--16 16 SeptemberSeptember 20112011
- Historic background of the TFRM
- Preliminary SST results
- TFRM refurbishment project
- First year of TFRM operations
- First SST observations
- Immediate plans
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Historic background of TFRMHistoric background of TFRM- 21 Baker-Nunn Cameras (BNCs) were constructed by the
Smithsonian Institution on early 60s for satellites photographicobservation.
- One BNC was installed at ROA in 1958.
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
- After GEODSS program superseded BNCs, ROA BNC was donated to this institution.
- ROA BNC remained inactive since 80s.
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Ref.Proj.: mechanical modificationsRef.Proj.: mechanical modifications- Conversion of altazimuthal to
equatorial mount.
- Design and building of spidervanes which supports correctiveoptics, CCD, and focus motor(~10µm error).
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
- Hour angle and declination
axes are servo driven with
absolute encoders feedback.
- 3D tip-tilters for accuratecollimation of the system.
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Ref.Proj.: oRef.Proj.: optics refiguringptics refiguring
- Original focal plane is
curved
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
- A new two-element
corrective optics has
been added
- The outermost surface
of the 0.5m corrector
plate is repolished and
MgF2 coated
- 0.78m primary mirror is
realuminizated
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Ref.Proj.: oRef.Proj.: optics refiguring (II)ptics refiguring (II)
CaF field flattener lens Ellipsoidal corrective meniscus Color filter
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
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Ref.Proj.: oRef.Proj.: optics refiguring (III)ptics refiguring (III)
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
DiamondBrite©
(97% reflectivity) and
high durability
BEFORE AFTER
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Ref.Proj.: oRef.Proj.: optics refiguring (IV)ptics refiguring (IV)
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
BEFORE AFTER
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Ref.Proj.: cRef.Proj.: custom CCDustom CCD
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
- CCD custom designed by FLI
- 4096x4096 9µm pixel CCD
- CCD FoV is 4.4ºx4.4º. Scale of 3.88arcsec/pixel
- Field flattener lens is only 0.65mm over the CCD chip
- CCD chip is Peltier cooled. Heat is pumped out the tube by
refrigerated glycol recirculation
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Ref.Proj.: oRef.Proj.: observatory Control Softwarebservatory Control Software- Based on Instrument-Neutral
Distributed Interface (INDI) protocol,
created by Elwood C. Downey (Clear
Sky Institute, Inc.)
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
- INDI allows remote and robotic
control of every observatory device from
custom Java clients and schedulers
- Complex decisions can be
automatically taken in basis of
circumstances (weather, target
visibility, etc.), with user high-level
scripts (Python, Perl, bash)
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Ref.Proj.: bRef.Proj.: before and afterefore and after
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
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Ref.Proj.: sRef.Proj.: specifications comparisonpecifications comparison
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
MechanicsMechanicsMechanicsMechanics
Mount typeMount typeMount typeMount type AltazimutalAltazimutalAltazimutalAltazimutal
AzimuthAzimuthAzimuthAzimuth ManualManualManualManual
ElevationElevationElevationElevation ManualManualManualManual
OpticsOpticsOpticsOptics
DesignDesignDesignDesign Original BakerOriginal BakerOriginal BakerOriginal Baker----Nunn:Nunn:Nunn:Nunn:Modified Schmidt with sphericalModified Schmidt with sphericalModified Schmidt with sphericalModified Schmidt with sphericalmirror and 3mirror and 3mirror and 3mirror and 3----element plateelement plateelement plateelement platecorrectorcorrectorcorrectorcorrector
ApertureApertureApertureAperture 0.5m0.5m0.5m0.5m
Focal ratioFocal ratioFocal ratioFocal ratio f/1f/1f/1f/1
ScaleScaleScaleScale 410arcsec/mm410arcsec/mm410arcsec/mm410arcsec/mm
Primary mirrorPrimary mirrorPrimary mirrorPrimary mirror 0.78m0.78m0.78m0.78m
Campo visualCampo visualCampo visualCampo visual 5deg x 30deg5deg x 30deg5deg x 30deg5deg x 30deg
Spot sizeSpot sizeSpot sizeSpot size <20<20<20<20µµµµmmmm throughout the FoVthroughout the FoVthroughout the FoVthroughout the FoV
DetectorDetectorDetectorDetector
DetectorDetectorDetectorDetector Cinemascope filmCinemascope filmCinemascope filmCinemascope film
MechanicsMechanicsMechanicsMechanics
Mount typeMount typeMount typeMount type EcuatorialEcuatorialEcuatorialEcuatorial
Hour angleHour angleHour angleHour angle Digital servo driven motorsDigital servo driven motorsDigital servo driven motorsDigital servo driven motors
DeclinationDeclinationDeclinationDeclination Digital servo driven motorsDigital servo driven motorsDigital servo driven motorsDigital servo driven motors
OpticsOpticsOpticsOptics
DesignDesignDesignDesign BakerBakerBakerBaker----Nunn with correctiveNunn with correctiveNunn with correctiveNunn with correctiveoptics: field flattener andoptics: field flattener andoptics: field flattener andoptics: field flattener andmeniscus meniscus meniscus meniscus
ApertureApertureApertureAperture 0.5m0.5m0.5m0.5m
Focal ratioFocal ratioFocal ratioFocal ratio f/0.96f/0.96f/0.96f/0.96
ScaleScaleScaleScale 3.88arcsec/pixel3.88arcsec/pixel3.88arcsec/pixel3.88arcsec/pixel
Primary mirrorPrimary mirrorPrimary mirrorPrimary mirror 0.78m0.78m0.78m0.78m
CCD FoVCCD FoVCCD FoVCCD FoV 4.41deg x 4.41deg4.41deg x 4.41deg4.41deg x 4.41deg4.41deg x 4.41deg
Spot sizeSpot sizeSpot sizeSpot size <20<20<20<20µµµµmmmm throughout the FoVthroughout the FoVthroughout the FoVthroughout the FoV
DetectorDetectorDetectorDetector
SensorSensorSensorSensor Kodak KAFKodak KAFKodak KAFKodak KAF----16803, 4kx4k, 916803, 4kx4k, 916803, 4kx4k, 916803, 4kx4k, 9µµµµmmmm
CCD QECCD QECCD QECCD QE 60% a 550nm60% a 550nm60% a 550nm60% a 550nm
CameraCameraCameraCamera FLI PL16803, custom designFLI PL16803, custom designFLI PL16803, custom designFLI PL16803, custom design
Original BNC Refurbished TFRM
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First year of the TFRM operationsFirst year of the TFRM operations
- Since then, intensive testing under commissioning period.
TFRM conducted numerous programs: detection of exoplanets, SST, NEOs, and γγγγ–ray optical counterparts monitoring.
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
- Early Sep 2010: installation of TFRM at Montsec Astronomical
Observatory (OAdM)
- 10 Sep 2010: collimation of TFRM
- 11 Sep 2010: first light of TFRM
- 16 Sep 2010: inauguration of TFRM
- Late Dec 2010: INDI control software tunning
- 07 Feb 2011: first remote observation
- 25 Feb 2011: first unsupervised robotic observation
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First SST observationsFirst SST observationsTFRM specifications make an efficient facility to track and
survey from faint GEOs to fast LEOs objects:
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
- Moderate limiting magnitude (V~20mag ≡ 15cm size @ GEO
orbit) with 30s integration
- Huge FoV (4.4º x 4.4º) free of optical aberrations
- Arbitrary rate tracking simultaneously in RA and DEC (target
tracking by TLE specification)
- CCD shutter triggering several times at will during an exposure,
with 0.1ms timestamp accuracy
- Astrometric accuracies of 0.25arcsec for point-like objects
- Astrometric accuracies of 0.5arcsec for trailed stars
- Fully robotic telescope
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First SST observations (II)First SST observations (II)GEOs TRACKING observations:
- TFRM participated in the 3rd run of the ESA CO-VI satellite
tracking campaign of the SST/Space Surveillance Awareness
Preparatory Program (SST/SSA-PP).
- 13 telescopes and radars from different European countries
participated, coordinated by the Astronomical Institute University
of Bern (AIUB) office.
- From 30 Jan 2011 to 7 Feb 2011, TFRM conducted systematic
observations of artificial satellites to determine 1137 accurate
position measurements.
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
GEOs SURVEY observations:
- TFRM started to participate with ISON network as external
collaborator. Preliminary results are encouraging but still deserve
further observations to conclude survey efficiency, accuracy and
other key parameters.
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First SST observations (III)First SST observations (III)
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
NSS5: 5s exp.time
NAVSTAR/GPS: 5s exp.time
COSMOS 2333: 1s exp.time
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Preliminary SST resultsPreliminary SST results
AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
2-sigma (95%) uncertainties obtained over the MSG2 satellite, with 175 angular
measurements along the 4-night interval. Mean uncertainties in the classical
elements (semiaxis, eccentricity and inclination), are of the order of 12m, 1.8�10-6
and 1.5�10-4deg respectively.
Computation of Orbit Determination from the angular measurements
of the ESA CO-IV SST observations with Orbit Determination Tool
Kit (ODTK) software package (AGI).
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Immediate plansImmediate plans
AMOS 2011, 13AMOS 2011, 13--16 16 SeptemberSeptember 20112011
- Some hardware and software upgrades are currently
being carried out at the TFRM.
- We plan to calibrate our GEO tracking performance
through the intensive observation of known GEO
satellites and the comparison with the orbital
elements provided by the Satellite Control Agencies
(EUMETSAT, HISPASAT).
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AMOS 2011, 13AMOS 2011, 13--16 September 201116 September 2011
Thank you!Thank you!