Sensitivity ANALYSIS Sébastien Wagner (EUMETSAT) In collaboration with

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Sensitivity ANALYSIS Sébastien Wagner (EUMETSAT) In collaboration with Tom Stone (USGS) Sophie Lachérade, Bertrand Fougnie (CNES) Jack Xiong (NASA) With the great support of B. Viticchie, M. Takahashi, T. Hewison

What do we want to achieve? Needs: For users to know how reliable is the information they look at... For the developers to understand where systems / processing are critical (characterization, accuracy, stability)  tell where improvements can be done and what is the impact For calibration / inter-calibration: need to look at Acquisition chain Processing algorithms / methods Reference uncertainties Goal of the sensitivity analysis w.r.t. Lunar Calibration Workshop: Raise awareness about understanding the typical uncertainties on the input data Show how GIRO results vary by changing the input data. Initiate discussion on how to establish a uncertainty budget (to support calibration/inter-calibration products and their quality assessment) Not meant to be exhaustive and complete. It is mainly to start the process and exchange experience and knowledge...

Data source, measurement technique Dark signal correction Sensitivity tree Data source, measurement technique Source of degradation: Out of band rejection On-orbit degradation Non-linearity Spectral response Dark signal correction Oversampling Integration step Absolute calibration Data source Sensitivity study parameters ΔSRF ΔI Δ(x,y,z) SRF Sensor Irradiances Satellite position GIRO inputs GIRO

Sensitivity analysis... It is all about perturbation...

Data source, measurement technique Dark signal correction Sensitivity tree Data source, measurement technique Source of degradation: Out of band rejection On-orbit degradation Non-linearity Spectral response Dark signal correction Oversampling Integration step Absolute calibration Data source Sensitivity study parameters ΔSRF ΔI Δ(x,y,z) SRF Sensor Irradiances Satellite position GIRO inputs GIRO

Data source, measurement technique Dark signal correction Sensitivity tree Data source, measurement technique Source of degradation: Out of band rejection On-orbit degradation Non-linearity Spectral response Dark signal correction Oversampling Integration step Absolute calibration Data source Sensitivity study parameters Achievable only when imagettes are available or at image processing time at home! ΔSRF ΔI Δ(x,y,z) SRF Sensor Irradiances Satellite position GIRO inputs GIRO

Perturbation tool and sensitivity analysis Tool developed at EUMETSAT in C  the GIRO PERTurbation tool (GIRO_PERT) Currently four tests implemented to test the sensitivity of the GSICS Implementation of the ROLO model to: random perturbation of the satellite position, rigid shift of the SRF (for the tests, done in both directions [short WL, long WL]), change in the wavelength sampling of the SRF (by removing SRF information), and random perturbation of the SRF shape. Sensitivity assessment done using the ROLO reference irradiance and the phase angle Set-up = pre-defined list of images from each data set = input Each input is perturbed by selecting the type of perturbation Re-generation of a dummy input to the GIRO and extraction of the relevant output for the analysis. Runs managed by a shell script Should run on participants’ systems as it is built as the GIRO. TO BE TESTED.

Typical results post-processing – Satellite position Random perturbation along x, y, and z with uniform distribution between [ -500, 500] m, 100 runs, ΔIrr is the difference between the unperturbed irradiance and the perturbed ones.

Typical results post-processing – Rigid SRF shift Rigid shift of the SRF: an example from a run (red = original, black = modified) 6 shifts of the SRF (i.e., 6 runs) ΔIrr is the difference between the unperturbed irradiance and the perturbed ones.

Typical results post-processing – change on SRF sampling Change of sampling of the SRF: an example from a run (red = original, black = modified) 3 runs performed after keeping a SRF point every 4, 5, and 6 wavelengths. ΔIrr is the difference between the unperturbed irradiance and the perturbed ones.

Typical results post-processing – Noise on the SRF Change of shape of the SRF: an example from a run (red = original, black = modified) Random noise added to the SRF at each wavelength point with uniform distribution between [-0.05, 0.05], 100 runs, ΔIrr is the difference between the unperturbed irradiance and the perturbed ones.

OVERALL CONCLUSION Conclusion We have a tool to start sensitivity analysis activities Participants to estimate typical uncertainties on the set of parameters required by Lunar Calibration (including image processing) Be ready for brain storming and discussion on the topic: is what we do valid? Enough? What should be addressed? How? When? Etc. OVERALL CONCLUSION Lunar calibration Workshop = place for exchanging, discussing, comparing ways of addressing data preparation and data handling, and having a critical view on how to make the best use of the data. Plenty of slots for exchanging opinions and ideas Understanding better goes with sharing openly also problems and issues We learn better from mistakes Please, show us images from your instruments especially if they are not nice  But nice pictures are also granted 

Don’t forget gloves and warm socks