Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC...
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Transcript of Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC...
![Page 1: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/1.jpg)
Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight 1423C. Duroure, A. Delplanque (LaMP), M. Weber (AIRBUS)
1- We present a simple method to find the best mass to diameter function for a given sample set of hydrometeor images using as reference a alternate TWC measurement (in this case the hot wire Robust probe)2- We compare the TWC estimation using this method with other methods (method using only the total count, methods using classical power law fit, method using estimation with more geometrical parameters (Lawson & Baker, JAMC,2006)3- Examples of sampled images (capped columns) => simple geometrical model4- Work in progress:
Technical trouble:1-Small particles PSD (D<100µm). Trouble in the ROI code ?
2-Sensibility of the results to the threshold rules (example of PSD with decreasing threshold)
HAIC working document 18/11/2013 meeting
![Page 2: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/2.jpg)
TWC hot wire (Robust)
Best A.M estimateB
Lawson & B. estimate
Ctot estimate
Three exemples of TWC estimations from imager using different rules, compared to hot wire probe.
1
2
3
![Page 3: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/3.jpg)
1 2 3
Scatter plot (TWC from imager, TWC from hot wire probe)1- Best estimation using power law functions (see next slides)2- Lawson and Baker geometrical estimation f(A,W,L,P) (non linearity, due to Lmax estimation ?)3- Simplest estimation (using total count of hydrometeor images)
Comparisons between imager and hot wire probe
![Page 4: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/4.jpg)
Sigma using only total concentration
Best estimation using PSD and M(D) power law Beta=1.93
B=1.93B=1.50 B=2.50
1- Look for the best linear correlation of TWC from imager and hot wire (not sensible to theA prefactor, i.e. calibration factors, DOF,….) => Estimation of B
Estimation of the mass(diameter) function mass=A*Diam^B
![Page 5: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/5.jpg)
Step 2- Look for the best PDF correlation between the two probes Empirical estimation of the prefactor M= 3.28e-5 DsurStep 3- Verify the estimated mass to diameter law (Mass=A.DB)
assuming: shape model and hydrometeor density
- Imager… Hot wire
1.93
![Page 6: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/6.jpg)
Capped columns Leg [12 h,12.7 h]
Best estimate of B=1.93
Irregular+agregatesLeg [12.7 h,12.8 h]
Best estimate of B=1.98(more dense objects ?)
![Page 7: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/7.jpg)
Some examples of « well oriented » images of capped columns(more than 300 avaiable (D> 300µm) for the 10.6 Km leg [12h,12.7h]Manual estimation of 4 geometrical variables: (Lc,Wc) columns part, (Lp,Wp) plates part
1 mm
Lc
Wc
Lp
WpAssumed growth historie of these CP:1- Start as column for higth sursatuation S2- Transition to plate for low SLarge variability observed for this transition=> Dificult to define a « standard » shape
![Page 8: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/8.jpg)
Some examples of « irregular» images (+aggregates+rosettes) for the 10.6 Km altitude sub-leg [12.7 h,12.8h] (« old » region, low concentration)
1 mm
Assumed growth historie of these cristal ?1- Nucleation of supercooled droplet2- Vapour diffusion process (low S ?)2- Agregation
On the site: CATROI_V1423allCatalogue of all ROI images of size largerthan 300µm (for identification of regions)
![Page 9: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/9.jpg)
Tresholding sensibility analysis
Treshold definition:
Amp=(max(image)-min(image))/2Med= min(image)+AmpTresh=med-S*Amp
Binary image= image LE TreshS=0
S=0.1
S=0.2
S=0.25
GEO ROI files on the siteV1423_GEO_S000 S=0V1423_GEO_S010 S=0.1 ---------------V1423_GEO_S030 S=0.3
![Page 10: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/10.jpg)
S=0
S=0.1
S=0.2
S=0.25
2 pix
S=0
S=0.1S=0.2
S=0.25
Tresholding sensibility analysis
Small diameter effect Large diameter effect Diameter measure shift (few pixel) Artefact for tail of large particles
![Page 11: Best estimation of a local mass to diameter function using imaging probe and hot-wire TWC measurement Case of the AIRBUS imager during the Cayenne flight.](https://reader030.fdocuments.us/reader030/viewer/2022032709/56649eb05503460f94bb5623/html5/thumbnails/11.jpg)
Technical trouble:1-Small particles PSD (D<100µm). Trouble in the ROI code ?2-AIRBUS PSD jump ?
Diameter (µm) Diameter (µm)
• AIRBUS PSD__ ROI PSD
?