lyra on-board proba2

18
LYRA on-board PROBA2 in-orbit operations and achievements M. Dominique, J.-F. Hochedez et al. PROBA2 Workshop ESTEC, 2010/06/22

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LYRA on-board PROBA2. in-orbit operations and achievements. M. Dominique, J.-F. Hochedez et al. PROBA2 Workshop ESTEC, 2010/06/22. Routine activities. Nominal acquisition: Unit2 Integration time = 50 ms Calibration Dark current LED signal Back-up acquisition - PowerPoint PPT Presentation

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Page 1: LYRA on-board PROBA2

LYRA on-board PROBA2

in-orbit operations and achievements

M. Dominique, J.-F. Hochedez et al.PROBA2 Workshop ESTEC, 2010/06/22

Page 2: LYRA on-board PROBA2

Routine activities

Nominal acquisition: Unit2 Integration time = 50 ms

Calibration Dark current LED signal

Back-up acquisition Acquisition with units1 and 3

Flat-field analysis Off-pointing sequence

Bake out - decontamination Switch on of heaters

(temperature reaches 50°C)

Nominal

Weekly

Monthly

Monthly

Once every 6 months

Page 3: LYRA on-board PROBA2

Nominal acquisition

Parameters of the mode

IT 50 ms

Unit(s) Unit 2

LED No

Remark IT up to 10ms have been tested

Page 4: LYRA on-board PROBA2

Flares

Lyra senses flares down to B1.5 at leastLYRA list of flares is in agreement with the

one of GOESAlways visible in the two XUV-EUV

channelsSome strong and impulsive flares are also

visible in Lyman-alpha, which can then be used as a precursor

Page 5: LYRA on-board PROBA2

Flares

M2.0 flare 2010/02/08 – 22h33

Page 6: LYRA on-board PROBA2

Calibration sequence

More than one orbit needed to MSM detectors to reach stabilization. No significant difference between the LED signal at the beginning of

the mission and the current one

→ the degradation is affecting the filters and not the detectors

Dark current

Dark current

VIS LED UV LED UV LED VIS LED

Page 7: LYRA on-board PROBA2

Back-up acquisition

UNIT 2 UNIT 1

Page 8: LYRA on-board PROBA2

Back-up acquisition

UNIT 2 UNIT 3

Page 9: LYRA on-board PROBA2

Flat-field paving

Paving step : 0.3° The Hz channel signal doesn’t fit the modeled behavior based on pre-launch flat-field measurements

slight imprinted degradation ???

Page 10: LYRA on-board PROBA2

Bake-out

AB + CD heaters on for 24h Temperature increase of 10°

No significant effect on the data

Next attempt: July 01

Page 11: LYRA on-board PROBA2

Specific campaigns

Occultations Sun-Moon eclipses

Stray light analysis

SDO/EVE cross-calibration

campaign

Every orbit till MarchJanuary 15 (annular from LYRA)

July 11 (partial from LYRA)

March 18-19(still under analysis)

May 3(still under analysis)

Page 12: LYRA on-board PROBA2

Occultations

Ly alphaHzAlZr

Attitude change

Lyman alpha completely absorbed

Contribution of longer wavelengths

Page 13: LYRA on-board PROBA2

Sun-Moon eclipse

Disappearance and appearance of the active region behind the lunar disk

Attitude change

Occultation

Page 14: LYRA on-board PROBA2

EVE aging effects are tracked by flying the same instruments on-board a rocket 1x/year LYRA cross-calibration campaign was scheduled during the first rocket flight

Cross-calibration with SDO/EVE

200 220

Page 15: LYRA on-board PROBA2

LYRA on-board PROBA2

ANNEXES

Page 16: LYRA on-board PROBA2

Auroral Oval

Perturbations appearing around 75° latitude

2-3 days after a CME, flare ...

Associated to geomagnetic perturbations

Only in Al and Zr

Spacecraft maneuvers

SAA

Page 17: LYRA on-board PROBA2

And a fifth channel at 17.4nm...

... called SWAP!

Page 18: LYRA on-board PROBA2

LY-TMR:

State of the data processing pipeline

LY-EDG

LY-BSDG

Telemetry packets

Raw data (in counts)

Lv1: Engineering data (in Hz)

fitsfits

fits

fits

Lv2: Calibrated data (in W/m²)

Other tools Higher level data products

Current state In the future

Not distributed Not distributed

Daily basis After each contact

Not available After each contact

Plots + flare list availableirregular

systematic