Closed gomezzz closed 2 years ago
Soooo, these results are from 3 different runs with identical simulation times and settings but different timesteps.
For completeness' sake, this is the used config (for dt = 5s
, for 1s and 10s iteration are adjusted accordingly.)
sim:
logLevel: info # Available levels are off, critical, err, warn, info, debug, trace
iterations: 6307200 # Number of simulation iterations
maxAltitude: 10000 # Maximum satellite altitude [km]
deltaT: 5.0 # [s]
prop: # Which propagation model components should be applied
useKEPComponent: true # Keplerian propagation
useJ2Component: true # J2 spherical harmonic approximation
useC22Component: true # C22 spherical harmonic approximation
useS22Component: true # S22 spherical harmonic approximation
useSOLComponent: true # Solar gravitational pull
useLUNComponent: true # Lunar gravitational pull
useSRPComponent: true # Solar radiation pressure
useDRAGComponent: true # Atmospheric drag
io:
output_file: output.csv # Output file name
posFileName: pos.csv # Name of the CSV file with satellite positions [km]
velFileName: v.csv # Name of the CSV file with satellite velocities [km/s]
#progressOutputFrequency : 50 # Frequency of writing iteration number and encounter info to std::out.
vtkWriteFrequency: 4000 # Frequency of writing to vtk file [iterations]
#constellationList: StarlinkGen1,100,7200 # ';'-seperated constellations consisting of path (to constellation directory), start time, duration
#constellationFrequency: 10 # Frequency of adding satellites to simulation [iterations]
autopas:
logLevel: off
cutoff: 80.0 # Cutoff for autopas force interaction
skin: 160.0 # twice the maximum distance a particle can travel between two list rebuilds
rebuildFrequency: 20
desiredCellsPerDimension: 32 # Desired number of cells per dimension
tuningMode: false
# Newton3: "enabled, disabled"
# DataLayout: "AoS, SoA"
# Container: "varVerletListsAsBuilt, verletListCells"
# Traversal: "vvl_as_build, vlc_c01, vlc_c18, vlc_sliced_balanced, vlc_slice_c02"
Waiting for #68 to analyze orbital elements vs conjunctions (we still have escaping particles atm)
Feature
Desired behavior
Same # of conjunction
What needs to be done
Run with different dt in cfg
How it can be tested
Run