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1.6.0-DEV-7d3dac44dc.log
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Julia Version 1.6.0-DEV.1148
Commit 7d3dac44dc (2020-10-06 21:26 UTC)
Platform Info:
OS: Linux (x86_64-pc-linux-gnu)
CPU: AMD EPYC 7502 32-Core Processor
WORD_SIZE: 64
LIBM: libopenlibm
LLVM: libLLVM-10.0.1 (ORCJIT, znver2)
Environment:
JULIA_DEPOT_PATH = ::/usr/local/share/julia
JULIA_NUM_THREADS = 2
Resolving package versions...
Installed Python_jll ── v3.8.1+3
Installed Xerces_jll ── v3.2.3+0
Installed CSPICE_jll ── v66.0.0+2
Installed XZ_jll ────── v5.2.4+3
Installed OpenSSL_jll ─ v1.1.1+5
Installed Zlib_jll ──── v1.2.11+16
Installed Libffi_jll ── v3.2.1+3
Installed GMAT ──────── v0.1.0
Installed Expat_jll ─── v2.2.7+5
Installed GMAT_jll ──── v2020.0.0+0
Installed Bzip2_jll ─── v1.0.6+4
Updating `~/.julia/environments/v1.6/Project.toml`
[af5f6e49] + GMAT v0.1.0
Updating `~/.julia/environments/v1.6/Manifest.toml`
[6e34b625] + Bzip2_jll v1.0.6+4
[07f52509] + CSPICE_jll v66.0.0+2
[2e619515] + Expat_jll v2.2.7+5
[af5f6e49] + GMAT v0.1.0
[5472d9e0] + GMAT_jll v2020.0.0+0
[e9f186c6] + Libffi_jll v3.2.1+3
[458c3c95] + OpenSSL_jll v1.1.1+5
[93d3a430] + Python_jll v3.8.1+3
[ffd25f8a] + XZ_jll v5.2.4+3
[637d83c4] + Xerces_jll v3.2.3+0
[83775a58] + Zlib_jll v1.2.11+16
[56f22d72] + Artifacts
[2a0f44e3] + Base64
[ade2ca70] + Dates
[b77e0a4c] + InteractiveUtils
[76f85450] + LibGit2
[8f399da3] + Libdl
[d6f4376e] + Markdown
[44cfe95a] + Pkg
[de0858da] + Printf
[3fa0cd96] + REPL
[9a3f8284] + Random
[ea8e919c] + SHA
[9e88b42a] + Serialization
[6462fe0b] + Sockets
[fa267f1f] + TOML
[cf7118a7] + UUIDs
[4ec0a83e] + Unicode
Testing GMAT
Status `/tmp/jl_yDNSJY/Project.toml`
[af5f6e49] GMAT v0.1.0
[8dfed614] Test
Status `/tmp/jl_yDNSJY/Manifest.toml`
[6e34b625] Bzip2_jll v1.0.6+4
[07f52509] CSPICE_jll v66.0.0+2
[2e619515] Expat_jll v2.2.7+5
[af5f6e49] GMAT v0.1.0
[5472d9e0] GMAT_jll v2020.0.0+0
[e9f186c6] Libffi_jll v3.2.1+3
[458c3c95] OpenSSL_jll v1.1.1+5
[93d3a430] Python_jll v3.8.1+3
[ffd25f8a] XZ_jll v5.2.4+3
[637d83c4] Xerces_jll v3.2.3+0
[83775a58] Zlib_jll v1.2.11+16
[56f22d72] Artifacts
[2a0f44e3] Base64
[ade2ca70] Dates
[b77e0a4c] InteractiveUtils
[76f85450] LibGit2
[8f399da3] Libdl
[56ddb016] Logging
[d6f4376e] Markdown
[44cfe95a] Pkg
[de0858da] Printf
[3fa0cd96] REPL
[9a3f8284] Random
[ea8e919c] SHA
[9e88b42a] Serialization
[6462fe0b] Sockets
[fa267f1f] TOML
[8dfed614] Test
[cf7118a7] UUIDs
[4ec0a83e] Unicode
Testing Running tests...
********************************************
*** GMAT Console Application
********************************************
General Mission Analysis Tool
Console Based Version
Build Date: Jan 1 1970 00:00:00
Moderator is updating data files...
Moderator is creating core engine...
Successfully set Planetary Source to use: DE405
Successfully set Planetary Source to use: DE405
Successfully set Planetary Source to use: DE405
Setting nutation file to /home/pkgeval/.julia/artifacts/57d26c5107adc743bdb2cba39400f8c164b6d085/gmat-data-2020a/planetary_coeff/NUTATION.DAT
Setting leap seconds file to /home/pkgeval/.julia/artifacts/57d26c5107adc743bdb2cba39400f8c164b6d085/gmat-data-2020a/time/tai-utc.dat
2020-10-07 06:08:24 GMAT Moderator successfully created core engine
Interpreting scripts from the file.
***** file: /home/pkgeval/.julia/packages/GMAT/yR7o4/test/test.script
Successfully set Planetary Source to use: DE405
Successfully set Planetary Source to use: DE405
*** WARNING *** The model file '../data/vehicle/models/aura.3ds' does not exist for the spacecraft 'geoSat'
Successfully interpreted the script
.................... Print out the whole sequence ........................................
Command::NoOp
Command::BeginMissionSequence
Command::Propagate
Command::Target
... branch 0::Vary
... branch 0::Maneuver
... branch 0::Propagate
... branch 0::Achieve
... branch 0::EndTarget
Command::Propagate
Command::Propagate
Command::Target
... branch 0::Vary
... branch 0::Vary
... branch 0::Maneuver
... branch 0::Propagate
... branch 0::Achieve
... branch 0::Achieve
... branch 0::EndTarget
Command::Target
... branch 0::Vary
... branch 0::Maneuver
... branch 0::Achieve
... branch 0::EndTarget
Command::Propagate
.................... End sequence ........................................................
Running mission...
Successfully set Planetary Source to use: DE405
Successfully set Planetary Source to use: DE405
Kernel /home/pkgeval/.julia/artifacts/57d26c5107adc743bdb2cba39400f8c164b6d085/gmat-data-2020a/planetary_ephem/spk/DE405AllPlanets.bsp has been loaded.
Kernel /home/pkgeval/.julia/artifacts/57d26c5107adc743bdb2cba39400f8c164b6d085/gmat-data-2020a/planetary_coeff/SPICEPlanetaryConstantsKernel.tpc has been loaded.
Kernel /home/pkgeval/.julia/artifacts/57d26c5107adc743bdb2cba39400f8c164b6d085/gmat-data-2020a/time/SPICELeapSecondKernel.tls has been loaded.
Kernel /home/pkgeval/.julia/artifacts/57d26c5107adc743bdb2cba39400f8c164b6d085/gmat-data-2020a/planetary_coeff/SPICEEarthPredictedKernel.bpc has been loaded.
Kernel /home/pkgeval/.julia/artifacts/57d26c5107adc743bdb2cba39400f8c164b6d085/gmat-data-2020a/planetary_coeff/SPICEEarthCurrentKernel.bpc has been loaded.
Kernel /home/pkgeval/.julia/artifacts/57d26c5107adc743bdb2cba39400f8c164b6d085/gmat-data-2020a/planetary_coeff/earth_latest_high_prec.bpc has been loaded.
Kernel /home/pkgeval/.julia/artifacts/57d26c5107adc743bdb2cba39400f8c164b6d085/gmat-data-2020a/planetary_coeff/SPICELunaCurrentKernel.bpc has been loaded.
Kernel /home/pkgeval/.julia/artifacts/57d26c5107adc743bdb2cba39400f8c164b6d085/gmat-data-2020a/planetary_coeff/SPICELunaFrameKernel.tf has been loaded.
********************************************************
*** Performing Differential Correction (using "DC")
*** 1 variables; 1 goals
Variables: TOI.Element1
Goals: geoSat.RMAG
SolverMode: Solve
********************************************************
DC Iteration 1; Nominal Pass
Variables: TOI.Element1 = 1
Goals and achieved values:
geoSat.RMAG Desired: 85000 Achieved: 11538.5153039 Variance: 73461.4846961
Completed iteration 1, pert 1 (TOI.Element1 = 1.0001)
DC Iteration 2; Nominal Pass
Variables: TOI.Element1 = 1.5
Goals and achieved values:
geoSat.RMAG Desired: 85000 Achieved: 16224.5280307 Variance: 68775.4719693
Completed iteration 2, pert 1 (TOI.Element1 = 1.5001)
DC Iteration 3; Nominal Pass
Variables: TOI.Element1 = 2
Goals and achieved values:
geoSat.RMAG Desired: 85000 Achieved: 24787.2044873 Variance: 60212.7955127
Completed iteration 3, pert 1 (TOI.Element1 = 2.0001)
DC Iteration 4; Nominal Pass
Variables: TOI.Element1 = 2.5
Goals and achieved values:
geoSat.RMAG Desired: 85000 Achieved: 45288.0637535 Variance: 39711.9362465
Completed iteration 4, pert 1 (TOI.Element1 = 2.5001)
DC Iteration 5; Nominal Pass
Variables: TOI.Element1 = 3
Goals and achieved values:
geoSat.RMAG Desired: 85000 Achieved: 158769.444666 Variance: -73769.4446665
Completed iteration 5, pert 1 (TOI.Element1 = 3.0001)
DC Iteration 6; Nominal Pass
Variables: TOI.Element1 = 2.90046475429
Goals and achieved values:
geoSat.RMAG Desired: 85000 Achieved: 107938.220381 Variance: -22938.2203813
Completed iteration 6, pert 1 (TOI.Element1 = 2.90056475429)
DC Iteration 7; Nominal Pass
Variables: TOI.Element1 = 2.8353275274
Goals and achieved values:
geoSat.RMAG Desired: 85000 Achieved: 88881.6415762 Variance: -3881.64157618
Completed iteration 7, pert 1 (TOI.Element1 = 2.8354275274)
DC Iteration 8; Nominal Pass
Variables: TOI.Element1 = 2.8193661454
Goals and achieved values:
geoSat.RMAG Desired: 85000 Achieved: 85155.3063629 Variance: -155.306362861
Completed iteration 8, pert 1 (TOI.Element1 = 2.8194661454)
DC Iteration 9; Nominal Pass
Variables: TOI.Element1 = 2.81867353247
Goals and achieved values:
geoSat.RMAG Desired: 85000 Achieved: 85000.3061658 Variance: -0.306165846021
Completed iteration 9, pert 1 (TOI.Element1 = 2.81877353247)
DC Iteration 10; Nominal Pass
Variables: TOI.Element1 = 2.81867216235
Goals and achieved values:
geoSat.RMAG Desired: 85000 Achieved: 85000.000066 Variance: -6.59993384033e-05
*** Targeting Completed in 10 iterations.
*** The Targeter converged!
Final Variable values:
TOI.Element1 = 2.81867216235
********************************************************
*** Performing Differential Correction (using "DC")
*** 2 variables; 2 goals
Variables: MCC.Element1, MCC.Element2
Goals: geoSat.EarthMJ2000Eq.INC, geoSat.RMAG
SolverMode: Solve
********************************************************
DC Iteration 1; Nominal Pass
Variables: MCC.Element1 = 0.1, MCC.Element2 = 0.1
Goals and achieved values:
geoSat.EarthMJ2000Eq.INC Desired: 2 Achieved: 22.3226227884 Variance: -20.3226227884
geoSat.RMAG Desired: 42195 Achieved: 8538.13325018 Variance: 33656.8667498
Completed iteration 1, pert 1 (MCC.Element1 = 0.1001)
Completed iteration 1, pert 2 (MCC.Element2 = 0.1001)
DC Iteration 2; Nominal Pass
Variables: MCC.Element1 = 0.6, MCC.Element2 = 0.256327741602
Goals and achieved values:
geoSat.EarthMJ2000Eq.INC Desired: 2 Achieved: 18.2845974337 Variance: -16.2845974337
geoSat.RMAG Desired: 42195 Achieved: 24212.9094223 Variance: 17982.0905777
Completed iteration 2, pert 1 (MCC.Element1 = 0.6001)
Completed iteration 2, pert 2 (MCC.Element2 = 0.256427741602)
DC Iteration 3; Nominal Pass
Variables: MCC.Element1 = 0.937961731506, MCC.Element2 = 0.733962093743
Goals and achieved values:
geoSat.EarthMJ2000Eq.INC Desired: 2 Achieved: 5.85105339637 Variance: -3.85105339637
geoSat.RMAG Desired: 42195 Achieved: 53427.9852237 Variance: -11232.9852237
Completed iteration 3, pert 1 (MCC.Element1 = 0.938061731506)
Completed iteration 3, pert 2 (MCC.Element2 = 0.734062093743)
DC Iteration 4; Nominal Pass
Variables: MCC.Element1 = 0.774251582476, MCC.Element2 = 0.804404993171
Goals and achieved values:
geoSat.EarthMJ2000Eq.INC Desired: 2 Achieved: 1.73929524215 Variance: 0.260704757855
geoSat.RMAG Desired: 42195 Achieved: 43664.019883 Variance: -1469.01988302
Completed iteration 4, pert 1 (MCC.Element1 = 0.774351582476)
Completed iteration 4, pert 2 (MCC.Element2 = 0.804504993171)
DC Iteration 5; Nominal Pass
Variables: MCC.Element1 = 0.760145431715, MCC.Element2 = 0.788194043041
Goals and achieved values:
geoSat.EarthMJ2000Eq.INC Desired: 2 Achieved: 2.00293591861 Variance: -0.00293591861237
geoSat.RMAG Desired: 42195 Achieved: 42220.8017593 Variance: -25.8017593189
Completed iteration 5, pert 1 (MCC.Element1 = 0.760245431715)
Completed iteration 5, pert 2 (MCC.Element2 = 0.788294043041)
DC Iteration 6; Nominal Pass
Variables: MCC.Element1 = 0.759781464903, MCC.Element2 = 0.788113772758
Goals and achieved values:
geoSat.EarthMJ2000Eq.INC Desired: 2 Achieved: 1.99999919152 Variance: 8.08478436642e-07
geoSat.RMAG Desired: 42195 Achieved: 42195.010066 Variance: -0.0100659910822
Completed iteration 6, pert 1 (MCC.Element1 = 0.759881464903)
Completed iteration 6, pert 2 (MCC.Element2 = 0.788213772758)
DC Iteration 7; Nominal Pass
Variables: MCC.Element1 = 0.759781349759, MCC.Element2 = 0.788113687532
Goals and achieved values:
geoSat.EarthMJ2000Eq.INC Desired: 2 Achieved: 1.99999999998 Variance: 2.17426077143e-11
geoSat.RMAG Desired: 42195 Achieved: 42195.0000008 Variance: -8.36487743072e-07
*** Targeting Completed in 7 iterations.
*** The Targeter converged!
Final Variable values:
MCC.Element1 = 0.759781349759
MCC.Element2 = 0.788113687532
********************************************************
*** Performing Differential Correction (using "DC")
*** 1 variables; 1 goals
Variables: MOI.Element1
Goals: geoSat.Earth.SMA
SolverMode: Solve
********************************************************
DC Iteration 1; Nominal Pass
Variables: MOI.Element1 = -0.1
Goals and achieved values:
geoSat.Earth.SMA Desired: 42166.9 Achieved: 57242.5935739 Variance: -15075.6935739
Completed iteration 1, pert 1 (MOI.Element1 = -0.0999)
DC Iteration 2; Nominal Pass
Variables: MOI.Element1 = -0.2
Goals and achieved values:
geoSat.Earth.SMA Desired: 42166.9 Achieved: 52144.5234844 Variance: -9977.62348441
Completed iteration 2, pert 1 (MOI.Element1 = -0.1999)
DC Iteration 3; Nominal Pass
Variables: MOI.Element1 = -0.3
Goals and achieved values:
geoSat.Earth.SMA Desired: 42166.9 Achieved: 47995.5748004 Variance: -5828.6748004
Completed iteration 3, pert 1 (MOI.Element1 = -0.2999)
DC Iteration 4; Nominal Pass
Variables: MOI.Element1 = -0.4
Goals and achieved values:
geoSat.Earth.SMA Desired: 42166.9 Achieved: 44557.5941019 Variance: -2390.69410193
Completed iteration 4, pert 1 (MOI.Element1 = -0.3999)
DC Iteration 5; Nominal Pass
Variables: MOI.Element1 = -0.476084013791
Goals and achieved values:
geoSat.Earth.SMA Desired: 42166.9 Achieved: 42314.8122252 Variance: -147.912225228
Completed iteration 5, pert 1 (MOI.Element1 = -0.475984013791)
DC Iteration 6; Nominal Pass
Variables: MOI.Element1 = -0.481432602619
Goals and achieved values:
geoSat.Earth.SMA Desired: 42166.9 Achieved: 42167.5548271 Variance: -0.654827079132
Completed iteration 6, pert 1 (MOI.Element1 = -0.481332602619)
DC Iteration 7; Nominal Pass
Variables: MOI.Element1 = -0.48145648872
Goals and achieved values:
geoSat.Earth.SMA Desired: 42166.9 Achieved: 42166.9000659 Variance: -6.59371944494e-05
*** Targeting Completed in 7 iterations.
*** The Targeter converged!
Final Variable values:
MOI.Element1 = -0.48145648872
Mission run completed.
===> Total Run Time: 1.900 seconds
========================================
*** GMAT Integration test (Console version) successful! ***
Moderator is deleting core engine...
Test Summary: | Pass Total
GMAT | 1 1
Testing GMAT tests passed