LIST OF PARAMETERS in MERGED FILES

If a NaN occurs in any of the columns it indicates there is no data, or no information for that time. i.e. When there is no LDAR data available (e.g. 000604), the column is replaced with NaN. If a single radar grid point did not have a valid return value NaN was used instead of a "bad data" value. In this way, the IDL code that does the plotting and other calculations could just skip over that point.

PARAMETER EXPLANATION
date flight day YYMMDD
HHMMSSbeginning time of 10 sec average in hours, minutes, seconds
sfmbeginning time of 10 sec average in seconds after midnight
x_pos x position of the A/C relative to WSR74C radar at PAFB
y_pos y position of the A/C relative to WSR74C radar at PAFB
POSLat A/C Latitude recorded by INS (2000) or Applanix (2001)
POSLong A/C Longitude recorded by INS or Applanix
POSRollbank angle of the A/C from INS or Applanix
POSPitchpitch angle of the A/C from INS or Applanix
POSHeadtrue heading from North of the A/C from INS or Applanix
POSAlt true altitude of the A/C from INS or Applanix [This altitude should be used for all analysis.]
TAS true airspeed of the A/C
PressAlt pressure altitude derived from the A/C measured temperature profile (differs from true altitude by about 300 to 500 m for ABFM altitudes)
Air_Temp air temperature measured by the Rosemount Temp. Sensor
LIQ_H2O Liquid Water Content measured by the King constant temp. sensor
Ice_D_LWC Supercooled liquid water detected by the Rosemount Ice Detector
Wind_M_Nose wind magnitude calculated from TAS measured by nose pitot
Wind_D_Nose wind direction from the nose pitot (meteorological sense)
Wind_Z_Nose vertical wind speed
Wind_M_Wing wind magnitude calculated from TAS measured by Wing pitot [The winds from WING pitot are not as reliable as from the NOSE and should be used only if user is convinced they seem reasonable.]
Wind_D_Wing wind direction from the Wing pitot
Turbulence epsilon**1/3 derived from the TAS
Con_FSSP Total part conc. from FSSP (see Microphysical Instrument Descriptions on the Report Page for description of all microphysical instruments.)
Tot_con_1DC Total part. conc. from PMS 1D probe
Tot_con_2DC Total part. conc. from PMS 2D probe
2DC_100_400 part. conc. from 100 to 400 microns from 2D probe
2DC_400_1000 part. conc. from 400 to 1000 microns from 2D probe
2DC_GT_1000 conc. of parts. > 1000 microns from 2D probe
ACP_2DC fraction of total parts. accepted in 2D processing -- a measure of probe performance; 1 = no problems
HVPS_GT_1000 conc. of parts. > 1000 microns from HVPS
HVPS_GT_3000 conc. of parts. > 3000 microns from HVPS
Ex_m x component of E field derived from M matrix solution
Ey_m y component of E field derived from M matrix solution
Ez_m z component of E field derived from M matrix solution
Eq_m E field due to charge on the aircraft
Em_m total magnitude of E field from M solution
EqdivbyEmag Eq divided by Emag; measure of quality of E measurement:
magnitude > 10 may be questionable.
DBZATAC reflectivity in the 1x1x1 km pixel at A/C location
COLFRAC1X1 fraction of pixels with detectable return &ge -10 dBZ in the single km column containing the aircraft from 5 km to 20 km
ColSum1x1 sum of dBZ with detectable return &ge -10dBZ in 1x1 column from z = 5 km up
COLFRAC1X1_0 the same as above except this is for detectable return &ge 0 dBZ
ColSum1x1_0 the same as above except this is for detectable return &ge 0 dBZ
NUM11x11 number of pixels with detectable return &ge -10dBZ in the 11x11 Column [the 11x11 Column extends 5 km N, S, W, and E of the 1x1 A/C location and from 5 to 20 km altitude.]
FRAC11X11 fraction of pixels with detectable return &ge -10 dBZ in the 11x11 Column
MAX11x11 maximum dBZ of any of the 1x1x1 pixels in the 11x11 Column
ALT_MAX11x11 altitude of the pixel with maximum dBZ in 11x11 Column
AVG11x11 average dBZ of all pixels with detectable return &ge -10 dBZ in 11x11 Column
THICK11x11 This is the difference of top11x11 - max(base11x11, 5km). So if the base is below 5 km the thickness is taken to be top - 5 km, if the base is greater than 5 km then thick = top - base. (with detectable return &ge -10 dBZ)
VOLINT11X11 avg11x11 x thick11x11
SDEV11x11 standard deviation of the dBZ average in the 11x11 Column (with detectable return &ge -10 dBZ)
TOP11x11 average altitude of the top of the cloud in the 11x11 Column
BASE11x11 average altitude of the base of the cloud in 11x11 Column. In order to avoid the existance of ground clutter, the logic was based on the column by column search for a base only if z > 2 km.
TOTSUM11X11 This is the sum of all of the detectable data points in the 11x11x(5:20km) column (with detectable return &ge -10 dBZ)
ACINTSUM11X11 ∑ [Avg(individual columns) * (columntop - columnbott + 1)]
the sum is over the columns of the 11x11 box (with detectable return &ge -10 dBZ)
SUMAVG11X11 horizontal averages were taken on each integer z-plane, then those values were summed. The averages were for &ge -10 dBZ.
(variable name)_0
If a variable name includes the _0 then it is the same calculation as for the variable name with the exception that the cutoff was for detectable returns &ge 0 dBZ
NUMCUBE3x3 number of pixels with detectable return in 3x3x3 km cube (for detectable returns &ge -10 dBZ)
MAXCUBE3X3 Maximum reflectivity value within the 3x3x3km cube (for detectable returns &ge -10 dBZ)
ALT_MAXCUBE3X3 The Altitude of the maximum reflectivity within the 3x3x3km cube (for detectable returns &ge -10 dBZ)
AVGCUBE3x3 average dBZ in the 3x3x3km cube (for detectable returns &ge -10 dBZ)
SDEVCUBE3x3 standard deviation of dBZ value of pixels in 3x3x3 cube (for detectable returns &ge -10 dBZ)
LDARm5 number of sources during this 10sec period within +/- 20 km and minus 5 min. of present A/C location/time.
CGm5 number of CG flashes from CGLSS within +/- 20 km and minus 5 min. of present A/C location/time.
LDARpm5 number of sources during 10 sec period within +/- 20 km and plus and minus 5 min. of present A/C location/time.
CGpm5 number of CG flashes from CGLSS within +/- 20 km and plus and 5 min. of present A/C location/time.
Etrans particle size in microns of the cross over between field driven and diffusive attachment [See Electrical Decay Model for Anvil Clouds> by John Willett in ABFM Reports on Web.]
ETmScl extrapolated time (secs) for decay of E field from 50 kV/m [See Report cited above.]
Cloud_Type type of anvil observed during this 10sec period:
0=no anvil
20=debris
10=distinct anvil with base >= 5 km altitude still attached to core
9=distinct anvil with base >= 5 km detached from core
8=anvil with particles measured but no detectable radar return
6=gnd clutter and other low altitude returns present, but still considered an anvil
4=Anvil with distinguishable base, but base below 5 km. Cases too far from radar to reliably determine base are excluded./td>
go to filter notes
Pass_num sequential number of pass for this flight; shown in the form pass#.anvil# e.g.
9.2 = pass #9 in anvil #2;
spirals are designated by an S on the end of this parameter, e.g.,
7.1S = pass # 7 in anvil #1 was a spiral
invoid_74C the A/C was in or within 10 km of the cone of silence at z = 10 km above the 74C radar
1=A/C in cone of silence
0=A/C not in cone of silence
invoid_88C as above but for the NEXRAD radar
core_20km A/C was within 20km of a convective core with reflectivity at 4km or higher of 35-40 dBZ or greater.
1=A/C is within 20 km of a core
0=A/C is not within 20 km of a core
atten_74C there was attenuation of the 74C radar by either intertevening precip or wet radome attenuation [See appropriate Reports and list of times on ABFM REPORTS web page.]
1=radar is attenuated
0=radar is not attenuated

 

 

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