XMM EPIC MOS Steve Sembay ([email protected]) Mallorca 01/04/09 A Phenomenological approach to the...

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XMM EPIC MOS Steve Sembay ([email protected]) Mallorca 01/04/09 A Phenomenological approach to the MOS detector response. Steve Sembay Phenomenological Theory. A theory which expresses mathematically the results of observed phenomena without paying detailed attention to their fundamental significance. i.e. If you don't understand it....describe it !

Transcript of XMM EPIC MOS Steve Sembay ([email protected]) Mallorca 01/04/09 A Phenomenological approach to the...

Page 1: XMM EPIC MOS Steve Sembay (sfs5@star.le.ac.uk) Mallorca 01/04/09 A Phenomenological approach to the MOS detector response. Steve Sembay Phenomenological.

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Steve Sembay ([email protected])Mallorca 01/04/09

A Phenomenological approach to the MOSdetector response.

Steve Sembay

Phenomenological Theory. A theory which expresses mathematically the results of observed phenomena without paying detailed attention to their fundamental significance.

i.e. If you don't understand it....describe it !

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Steve Sembay ([email protected])Mallorca 01/04/09

Motivation:

Develop a descriptive model of the RMF that is computationally quick to generate and provides a “reasonably” accuratedescription of the spatial and temporal variations observed in the MOS RMF (i.e. the patch)

A “quick” RMF makes deriving RMF parameters viaoptimisation procedures practical and allows one to providea description for changes to the RMF much more quickly than“manual tweaking”

Such a model could be used to inform a more physically realisticmodel.

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Steve Sembay ([email protected])Mallorca 01/04/09

tnmin optimisationprogram in IDL

IACHEC modelfor 1E0102

Automated RMF fitting

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Steve Sembay ([email protected])Mallorca 01/04/09

x (μm)1.0

0.0

f(x)

f(x) = α + (β E0)

E(x) = f(x) E0

I(e) = ∑I(x)exp(E(x),e,σ) dx

α = α(E0), β = β(E

0)

Current Empirical Surface Loss Model

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Steve Sembay ([email protected])Mallorca 01/04/09

Nov 1997 - FM1 = Flight Spare “Calibrate Orsay”

Apr 1998 – FM2 = MOS2 6 CCDs (1 faulty)Camera rebuild in June 1998

July 1998 – FM3 = MOS1 7 CCDs

Nov 1998 – FM1 = Flight Spare 7 CCDs

Orsay MOS Calibration Campaign

Data on 20 EPIC-MOS CCDsMOS1 - All 7 CCDs in orbit have Orsay ground cal dataMOS2 - Due to rebuild, 4 CCDs in orbit have Orsay ground cal data

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Steve Sembay ([email protected])Mallorca 01/04/09

FM1 MOS1 MOS2FM1 MOS1 MOS2FM1 MOS1 MOS2

Orsay Data

20 CCDs

Einput

= 350 eV

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Steve Sembay ([email protected])Mallorca 01/04/09

FM1 MOS1 MOS2FM1 MOS1 MOS2FM1 MOS1 MOS2

Orsay Data

20 CCDs

Einput

= 350 eV

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Steve Sembay ([email protected])Mallorca 01/04/09

Orsay Data

20 CCDs

Einput

= 350 eV

Re-order bystrength of losspeak.

“Good”

“Bad”

What if the way the shape changes from “good” to bad” from CCD to CCD (at a given energy) is similar to the way the shape

of the loss peak in the patch changes with time on the central CCD (at that energy).

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Steve Sembay ([email protected])Mallorca 01/04/09

Position and Size of Loss Component have relatively simplefunctional forms versus energy

0.73

MOS1CCD1

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Steve Sembay ([email protected])Mallorca 01/04/09

Position of loss peak / position of main peak

Fraction ofcounts in losspeak

These two quantities are correlated!

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Steve Sembay ([email protected])Mallorca 01/04/09

Position of loss peak / position of main peak

Fraction ofcounts in losspeak

These two quantities are correlated!

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Steve Sembay ([email protected])Mallorca 01/04/09

The position of the loss peak relative to the main peak(The Epeak parameter) is constant with energy (at leastabove ~300 eV)

The strength of loss peak follows a simple exponentialrelation with energy.

The normalisation of this relation is correlated with Epeak.

In this simple descriptive model, a single parameter, Epeakdefines the position and strength of the loss peak as a functionof energy.

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Steve Sembay ([email protected])Mallorca 01/04/09

Descriptive Model: The VRMF Model Main Peak

Blue Wing:Gaussian

Red Wing:Voigt Function

= Gaussian convolved with a Lorentian.

Dampening factor= 0 (Gaussian)> 0 (Lorentz-like)

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Steve Sembay ([email protected])Mallorca 01/04/09

Descriptive Model: The VRMF Model Loss Peak

Blue Wing:Triangular

Red Wing:Gaussian

Time to generate 2400 x 2400 SAS p0 rmf ~ 60 seconds

Time to generate 2400 x 2400 VRMF p0 rmf ~ 2 seconds

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Steve Sembay ([email protected])Mallorca 01/04/09

0065 1082 1165

Comparing the Model to 1E0102 (MOS1)

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Steve Sembay ([email protected])Mallorca 01/04/09

IACHEC modelfor 1E0102

Automated RMF fitting

Epeak

σ = a + b*sqrt(E)

Global Norm

4 Free Parameters

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Steve Sembay ([email protected])Mallorca 01/04/09

χ2 (SAS) χ2 (VRMF) EpeakRev 0065 2.45 2.40 0.78Rev 1082 4.06 2.01 0.70Rev 1165 5.02 1.78 0.46

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Steve Sembay ([email protected])Mallorca 01/04/09

χ2 (SAS) χ2 (VRMF) EpeakRev 0065 2.45 2.40 0.78Rev 1082 4.06 2.01 0.70Rev 1165 5.02 1.78 0.46

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Steve Sembay ([email protected])Mallorca 01/04/09

χ2 (SAS) χ2 (VRMF) EpeakRev 0065 2.45 2.40 0.78Rev 1082 4.06 2.01 0.70Rev 1165 5.02 1.78 0.46

c.f. Orsay Epeak = 0.73

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Steve Sembay ([email protected])Mallorca 01/04/09

Lines ~0.8-0.85 keV too strong ?

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Steve Sembay ([email protected])Mallorca 01/04/09

Conclusions:

1) It is possible to mathematically describe the energy dependentshape of the loss component of the RMF, as observed in our ground cal, with a model which has one dependent parameter = Epeak. (True > 300-350 eV)

2) Deriving Epeak assuming the IACHEC 1E0102 model givesvalues consistent with that measured at Orsay for off-axis andconsistent with our “picture” of the patch for on-axis.

3) What about low energies? Below ~300-350 eV

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Steve Sembay ([email protected])Mallorca 01/04/09

The Curious Case of Konrad's Comet

Obs:3.29 cts/s

Model:3.33 cts/s

χ2 = Bad!

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Steve Sembay ([email protected])Mallorca 01/04/09

The Curious Case of Konrad's Comet

Obs:3.25 cts/s

Model:3.37 cts/s

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Steve Sembay ([email protected])Mallorca 01/04/09

The Curious Case of Konrad's Comet

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Steve Sembay ([email protected])Mallorca 01/04/09

The Curious Case of Konrad's Comet

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Steve Sembay ([email protected])Mallorca 01/04/09

The Curious Case of Konrad's Comet

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Steve Sembay ([email protected])Mallorca 01/04/09

Orsay Data

20 CCDs

Einput

= 350 eV

Re-order bystrength of losspeak.

“Good”

“Bad”