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OSIRIS operation summary
In flight operations so far 3+1 commissioning slots (13 passes) Interference campaign Pointing and alignment scenario (11 observations with OSIRIS participation) Software update, DDS test Goals of operations Functional tests Calibration PR
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OSIRIS images in flight so far
Date Action Funct. tests Sync. tests Other calibs. Total 11-12 Mar Commissioning 1 13 - 28 41 25 Mar May Commissioning 2 964 64 125 1153 3-5 June Commissioning 2b 311 47 358 5 August DDS test 4-6 Sept. Software update 32 14-18 Sept. Commissioning 3 93 576 103 772 20-21 Sept. Interference 579 23-30 Sept. Pointing 18 312 330 1399 672 1194 3265
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CCD Calibrations Calibration Bias with warm and cold CCD
Covers all configurations except low power mode and dithering Additional subframe bias before stellar calibrations Full frame bias and dark images with s exposure time CCD sync tests
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NAC Dark image Lots of cosmics Note long stripe Several hot pixels
Exposure time 10 minutes Lots of cosmics Note long stripe Several hot pixels Apart from hot pixels very little dark current Weak horizontal noise pattern
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WAC dark image Lots of cosmics Several hot pixels
Exposure time 10 minutes Lots of cosmics Several hot pixels Apart from hot pixels very little dark current
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Internal lamps “Flat fields” with internal lamps with both cameras
1 uncompressed flat field for standard filter combination with main and redundant lamps Compressed (ratio 6) flat fields in “all” other non-UV filters Check of blocking of visible light in UV filters with uncompressed images, 8x8 binning
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NAC with calibration lamps
Orange filter, 2 sec. exposure Illumination not completely homogeneous No obvious difference to images from the ground Note intensity increase in first and last column
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WAC with calibration lamps
Red filter, 1.25 s exposure Illumination extremely inhomogeneous No difference from ground calibration visible Intensity increase in first and last column is present
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Calibrations with open doors
Stellar intensity calibrations ε Aqr, 59 Aql (secondary standards, early type) Vega (primary standard) 16 Cyg (solar type, WAC only) α Grus (very early type, Alice target, WAC only) Stars also useful for focus, PSF, and spacecraft pointing relative to OSIRIS “Random” star fields Geometric calibration, PSF, focus, spacecraft pointing Straylight at 90 deg. solar elongation WAC: Neptune in the field of view
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Vega with NAC and WAC NAC, Filter neutral-orange WAC, red filter
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NAC Starfield Orange filter, 5 sec exposure
Taken on June 5 Orange filter, 5 sec exposure Typical (not spectacular) field
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WAC Starfield Red filter, 30 s exposure Note the mysterious stripes
Note the presence of straylight
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Calibrations with open doors (2)
Planetary targets for solar-like calibration Earth and moon Venus Saturn and Titan Selected fields for geometric calibration M42 and environment for WAC Serves also for calibration of narrow band filters with line emissions Area 98 for NAC Also useful for PSF, focus, straylight,…
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Earth and Moon NAC NAC 3 color composite (blue, green, orange) Logarithmic representation (moon is much darker than earth)
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Earth and Moon WAC WAC Na filter, 0.5 s exposure time Logarithmic representation (moon is much darker than earth) Earth slightly overexposed
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Area 98 (NAC) Orange filter, 1 min exposure time
Rich field for accurate geometric calibration Telescope tracking appears to be bad
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M 42 (WAC) Na filter, 10 min exposure Logarithmic presentation
Orion nebula: Emissions + Continuum
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Straylight test PR Solar elongation 20 – 140 degrees covered
Also test of spacecraft pointing stability Strongly overexposed images of the Earth and the moon have been acquired during straylight test PR Comet LINEAR 2002 (T7) M42 Earth/moon system
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Straylight NAC Orange filter, solar elongation 70 degrees
15 s exposure time, binning 4x4 Overexposed earth offers nice opportunity to study ghosts
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Straylight WAC Red filter, solar elongation 70 degrees
0.75 s exposure time, binning 4x4 Straylight up to ~5000 counts in first rows (note binning, though) Ghosts of overexposed earth (and moon)
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OSIRIS NAC Multicolour Image
(blue, green, orange) Comet C/LINEAR 2002 T km distance – 1. May 2004
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NAC colour composite of M42
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Other Calibrations High-speed imaging test
Maximum image repetition rate Test of image transport through plainfile Handling of large data volumes Test of low power mode Test of transmission of science data through housekeeping link
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Current and future operations
Currently RSOC commissioning Test of interface experimenters/RSOC/(RMOC) Four “routine scenarios” for comet observations are simulated Dry test (no observations performed)
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Operations 2005 Earth flyby 1
~3000 km flyby distance from the Earth ~ km closest approach to the moon Observations of comet P/Tempel 1 during deep impact encounter (TBC) 2 payload checkouts
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Long term plans Taken from: Presentation by P. Ferri, ESOC
RVM RVM Lutetia Flyby 100710 Mars Flyby 250207 Earth Flyby Earth Flyby Steins Flyby 050908 Earth Flyby Comet Orbit Insertion Launch Landing Taken from: Presentation by P. Ferri, ESOC
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