Published April 17, 2024 | Version v1
Software Open

The Software for Modeling FETCH Observations of 2005 May 13 CME

  • 1. ROR icon Planetary Science Institute
  • 2. ACS Engineering & Safety
  • 3. University of Michigan
  • 4. ROR icon United States Naval Research Laboratory
  • 5. ROR icon Goddard Space Flight Center
  • 6. ROR icon University of Massachusetts Lowell

Description

The following MATLAB codes and inputs were used to create the majority of figures and tables in the **submitted** ApJ article (#AAS55701), "Modeling FETCH Observations of 2005 May 13 CME". 

Abstract

Coronal Mass Ejections (CMEs) evolve significantly as they propagate from the Sun to the Earth, so remote observations of changes in speed, strength of the magnetic field, density, and overall structure are critical for predicting their arrival time and geoeffectiveness. Radio remote observations of Faraday rotation and Total Electron Content combined with white-light observations enables the measurement of these properties with careful analyses. This paper describes the analysis techniques and evaluates their accuracy with regard to measuring a CME’s complex evolving structure and speed. The approach utilizes the layout of the Faraday effect tracker of coronal and heliospheric strutures (FETCH) with AWSoM simulations as input for evaluating these radio-based measures.

Archive Organization

MATLAB Code: VelTablesJensenEtAl.m - Generates data for Tables 1-3 and Figure 9 

Inputs:

Line1LineTimeArrive.csv - arrival time of signal traveling Line 1, [minutes] after beginning of simulation, irregular spacing (single column)
Line2LineTimeArrive.csv - same for Line 2
Line3LineTimeArrive.csv - same for Line 3
Line4LineTimeArrive.csv - same for Line 4

Line1ForwardTEC.csv - Total Electron Content [#/m^2] along Line 1 at time given in Line1LineTimeArrive (single column)
Line2ForwardTEC.csv - same for Line 2
Line3ForwardTEC.csv - same for Line 3
Line4ForwardTEC.csv - same for Line 4

Line1Forwardpath.csv - Locations of grid points [solar radii, Heliographic Inertial coordinate system, X-direction in column 1, Y-direction in column 2] for Line 1 path
Line2Forwardpath.csv - same for Line 2
Line3Forwardpath.csv - same for Line 3
Line4Forwardpath.csv - same for Line 4

Line1ForwardN.csv - Density [#/cm^3] at selected grid points along Line 1 at time given in Line1LineTimeArrive; rows delineate the grid (values at Line1Forwardpath locations) and columns for time (values at Line1LineTimeArrive) 
Line2ForwardN.csv - same for Line 2
Line3ForwardN.csv - same for Line 3
Line4ForwardN.csv - same for Line 4

Line1ForwardVx.csv - Velocity [km/sec] in the X-direction at each grid point along Line 1 at time given in Line1LineTimeArrive; rows delineate the grid (values at Line1Forwardpath locations) and columns for time (values at Line1LineTimeArrive) 
Line2ForwardVx.csv - same for Line 2
Line3ForwardVx.csv - same for Line 3
Line4ForwardVx.csv - same for Line 4

Line1ForwardVy.csv - Velocity [km/sec] in the Y-direction at each grid point along Line 1 at time given in Line1LineTimeArrive; rows delineate the grid (values at Line1Forwardpath locations) and columns for time (values at Line1LineTimeArrive) 
Line2ForwardVy.csv - same for Line 2
Line3ForwardVy.csv - same for Line 3
Line4ForwardVy.csv - same for Line 4

Line1ForwardRM.csv - Rotation measure [rad/m^2] along Line 1 at time given in Line1LineTimeArrive (single column)
Line2ForwardRM.csv - same for Line 2
Line3ForwardRM.csv - same for Line 3
Line4ForwardRM.csv - same for Line 4

MATLAB Code: AppBJensenEtAl.m - Generates Figures 7, 10, 16, 17, and data in Table 4

Inputs (previously described): Line1ForwardTEC (& Line2ForwardTEC, Line3ForwardTEC, and Line4ForwardTEC), Line1ForwardN (& Line2ForwardN, Line3ForwardN, and Line4ForwardN), Line1LineTimeArrive (& Line2LineTimeArrive, Line3LineTimeArrive, and Line4LineTimeArrive), Line1Forwardpath (& Line2Forwardpath, Line3Forwardpath, and Line4Forwardpath)

MATLAB Code: FETCHSimDataJensenEtAl.m - Generates Figures 8, 11, 12, 13, and 14

Inputs (previously described): Line1ForwardTEC (& Line2ForwardTEC, Line3ForwardTEC, and Line4ForwardTEC), Line1ForwardN (& Line2ForwardN, Line3ForwardN, and Line4ForwardN), Line1LineTimeArrive (& Line2LineTimeArrive, Line3LineTimeArrive, and Line4LineTimeArrive), Line1Forwardpath (& Line2Forwardpath, Line3Forwardpath, and Line4Forwardpath), Line1ForwardRM (& Line2ForwardRM, Line3ForwardRM, and Line4ForwardRM)

Line1ForwardBx.csv - Magnetic field [G] in the X-direction at each grid point along Line 1 at time given in Line1LineTimeArrive; rows delineate the grid (values at Line1Forwardpath locations) and columns for time (values at Line1LineTimeArrive) 
Line2ForwardBx.csv - same for Line 2
Line3ForwardBx.csv - same for Line 3
Line4ForwardBx.csv - same for Line 4

Line1ForwardBy.csv - Magnetic field [G] in the Y-direction at each grid point along Line 1 at time given in Line1LineTimeArrive; rows delineate the grid (values at Line1Forwardpath locations) and columns for time (values at Line1LineTimeArrive) 
Line2ForwardBy.csv - same for Line 2
Line3ForwardBy.csv - same for Line 3
Line4ForwardBy.csv - same for Line 4

Files

LineForwardBxBy.zip

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Additional details

Funding

Goddard Space Flight Center
George Mason University - PHaSER PHaSER
Goddard Space Flight Center
MOST/FETCH Antenna Engineering Design Development Software & Hardware 80NSSC21K1991
National Aeronautics and Space Administration
STEREO mission and HGI 80NSSC23K0447

Dates

Submitted
2024-05-14
Production of the code for submission to ApJ

Software

Programming language
MATLAB