Package evaluation of GMAT on Julia 1.11.4 (a71dd056e0*) started at 2025-04-08T09:26:38.399


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# Set-up
#

Installing PkgEval dependencies (TestEnv)...

Set-up completed after 8.95s


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# Installation
#

Installing GMAT...
   Resolving package versions...
    Updating `~/.julia/environments/v1.11/Project.toml`
  [af5f6e49] + GMAT v0.1.0
    Updating `~/.julia/environments/v1.11/Manifest.toml`
  [af5f6e49] + GMAT v0.1.0
  [692b3bcd] + JLLWrappers v1.7.0
  [21216c6a] + Preferences v1.4.3
  [6e34b625] + Bzip2_jll v1.0.9+0
  [07f52509] + CSPICE_jll v67.0.0+0
  [2e619515] + Expat_jll v2.6.5+0
  [5472d9e0] + GMAT_jll v2020.0.0+0
  [7106de7a] + LibMPDec_jll v2.5.2+0
  [e9f186c6] + Libffi_jll v3.4.7+0
  [458c3c95] + OpenSSL_jll v3.0.16+0
  [93d3a430] + Python_jll v3.10.16+0
  [76ed43ae] + SQLite_jll v3.48.0+0
  [ffd25f8a] + XZ_jll v5.8.1+0
  [637d83c4] + Xerces_jll v3.2.4+0
  [0dad84c5] + ArgTools v1.1.2
  [56f22d72] + Artifacts v1.11.0
  [2a0f44e3] + Base64 v1.11.0
  [ade2ca70] + Dates v1.11.0
  [f43a241f] + Downloads v1.6.0
  [7b1f6079] + FileWatching v1.11.0
  [b27032c2] + LibCURL v0.6.4
  [76f85450] + LibGit2 v1.11.0
  [8f399da3] + Libdl v1.11.0
  [56ddb016] + Logging v1.11.0
  [d6f4376e] + Markdown v1.11.0
  [ca575930] + NetworkOptions v1.2.0
  [44cfe95a] + Pkg v1.11.0
  [de0858da] + Printf v1.11.0
  [9a3f8284] + Random v1.11.0
  [ea8e919c] + SHA v0.7.0
  [fa267f1f] + TOML v1.0.3
  [a4e569a6] + Tar v1.10.0
  [cf7118a7] + UUIDs v1.11.0
  [4ec0a83e] + Unicode v1.11.0
  [deac9b47] + LibCURL_jll v8.6.0+0
  [e37daf67] + LibGit2_jll v1.7.2+0
  [29816b5a] + LibSSH2_jll v1.11.0+1
  [c8ffd9c3] + MbedTLS_jll v2.28.6+0
  [14a3606d] + MozillaCACerts_jll v2023.12.12
  [83775a58] + Zlib_jll v1.2.13+1
  [8e850ede] + nghttp2_jll v1.59.0+0
  [3f19e933] + p7zip_jll v17.4.0+2

Installation completed after 1.98s


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# Precompilation
#

Precompiling PkgEval dependencies...

Precompiling package dependencies...

Precompilation completed after 27.26s


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# Testing
#

     Testing GMAT
      Status `/tmp/jl_8vygMY/Project.toml`
  [af5f6e49] GMAT v0.1.0
  [8dfed614] Test v1.11.0
      Status `/tmp/jl_8vygMY/Manifest.toml`
  [af5f6e49] GMAT v0.1.0
  [692b3bcd] JLLWrappers v1.7.0
  [21216c6a] Preferences v1.4.3
  [6e34b625] Bzip2_jll v1.0.9+0
  [07f52509] CSPICE_jll v67.0.0+0
  [2e619515] Expat_jll v2.6.5+0
  [5472d9e0] GMAT_jll v2020.0.0+0
  [7106de7a] LibMPDec_jll v2.5.2+0
  [e9f186c6] Libffi_jll v3.4.7+0
  [458c3c95] OpenSSL_jll v3.0.16+0
  [93d3a430] Python_jll v3.10.16+0
  [76ed43ae] SQLite_jll v3.48.0+0
  [ffd25f8a] XZ_jll v5.8.1+0
  [637d83c4] Xerces_jll v3.2.4+0
  [0dad84c5] ArgTools v1.1.2
  [56f22d72] Artifacts v1.11.0
  [2a0f44e3] Base64 v1.11.0
  [ade2ca70] Dates v1.11.0
  [f43a241f] Downloads v1.6.0
  [7b1f6079] FileWatching v1.11.0
  [b77e0a4c] InteractiveUtils v1.11.0
  [b27032c2] LibCURL v0.6.4
  [76f85450] LibGit2 v1.11.0
  [8f399da3] Libdl v1.11.0
  [56ddb016] Logging v1.11.0
  [d6f4376e] Markdown v1.11.0
  [ca575930] NetworkOptions v1.2.0
  [44cfe95a] Pkg v1.11.0
  [de0858da] Printf v1.11.0
  [9a3f8284] Random v1.11.0
  [ea8e919c] SHA v0.7.0
  [9e88b42a] Serialization v1.11.0
  [fa267f1f] TOML v1.0.3
  [a4e569a6] Tar v1.10.0
  [8dfed614] Test v1.11.0
  [cf7118a7] UUIDs v1.11.0
  [4ec0a83e] Unicode v1.11.0
  [deac9b47] LibCURL_jll v8.6.0+0
  [e37daf67] LibGit2_jll v1.7.2+0
  [29816b5a] LibSSH2_jll v1.11.0+1
  [c8ffd9c3] MbedTLS_jll v2.28.6+0
  [14a3606d] MozillaCACerts_jll v2023.12.12
  [83775a58] Zlib_jll v1.2.13+1
  [8e850ede] nghttp2_jll v1.59.0+0
  [3f19e933] p7zip_jll v17.4.0+2
     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
2025-04-08 09:27:28 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 = 2.90046475428
   Goals and achieved values:
      geoSat.RMAG  Desired: 85000  Achieved: 107938.220374  Variance: -22938.2203743

   Completed iteration 6, pert 1 (TOI.Element1 = 2.90056475428)

DC Iteration 7; Nominal Pass
   Variables:  TOI.Element1 = 2.83532754635
   Goals and achieved values:
      geoSat.RMAG  Desired: 85000  Achieved: 88881.6461845  Variance: -3881.64618449

   Completed iteration 7, pert 1 (TOI.Element1 = 2.83542754635)

DC Iteration 8; Nominal Pass
   Variables:  TOI.Element1 = 2.81936615405
   Goals and achieved values:
      geoSat.RMAG  Desired: 85000  Achieved: 85155.3082976  Variance: -155.308297578

   Completed iteration 8, pert 1 (TOI.Element1 = 2.81946615405)

DC Iteration 9; Nominal Pass
   Variables:  TOI.Element1 = 2.8186735327
   Goals and achieved values:
      geoSat.RMAG  Desired: 85000  Achieved: 85000.3062023  Variance: -0.306202335079

   Completed iteration 9, pert 1 (TOI.Element1 = 2.8187735327)

DC Iteration 10; Nominal Pass
   Variables:  TOI.Element1 = 2.81867216243
   Goals and achieved values:
      geoSat.RMAG  Desired: 85000  Achieved: 85000.0000883  Variance: -8.83436441654e-05


*** Targeting Completed in 10 iterations.
*** The Targeter converged!
Final Variable values:
   TOI.Element1 = 2.81867216243

********************************************************
*** 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: 22.3226227875  Variance: -20.3226227875
      geoSat.RMAG  Desired: 42195  Achieved: 8538.13325061  Variance: 33656.8667494

   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 = 0.25632774108
   Goals and achieved values:
      geoSat.EarthMJ2000Eq.INC  Desired: 2  Achieved: 18.2845974534  Variance: -16.2845974534
      geoSat.RMAG  Desired: 42195  Achieved: 24212.9094235  Variance: 17982.0905765

   Completed iteration 2, pert 1 (MCC.Element1 = 0.6001)
   Completed iteration 2, pert 2 (MCC.Element2 = 0.25642774108)

DC Iteration 3; Nominal Pass
   Variables:  MCC.Element1 = 0.937961731479, MCC.Element2 = 0.733962093535
   Goals and achieved values:
      geoSat.EarthMJ2000Eq.INC  Desired: 2  Achieved: 5.85105340088  Variance: -3.85105340088
      geoSat.RMAG  Desired: 42195  Achieved: 53427.9852355  Variance: -11232.9852355

   Completed iteration 3, pert 1 (MCC.Element1 = 0.938061731479)
   Completed iteration 3, pert 2 (MCC.Element2 = 0.734062093535)

DC Iteration 4; Nominal Pass
   Variables:  MCC.Element1 = 0.774251582372, MCC.Element2 = 0.804404993086
   Goals and achieved values:
      geoSat.EarthMJ2000Eq.INC  Desired: 2  Achieved: 1.73929524175  Variance: 0.260704758247
      geoSat.RMAG  Desired: 42195  Achieved: 43664.0198875  Variance: -1469.01988751

   Completed iteration 4, pert 1 (MCC.Element1 = 0.774351582372)
   Completed iteration 4, pert 2 (MCC.Element2 = 0.804504993086)

DC Iteration 5; Nominal Pass
   Variables:  MCC.Element1 = 0.760145431567, MCC.Element2 = 0.788194042924
   Goals and achieved values:
      geoSat.EarthMJ2000Eq.INC  Desired: 2  Achieved: 2.00293591852  Variance: -0.0029359185221
      geoSat.RMAG  Desired: 42195  Achieved: 42220.8017594  Variance: -25.8017594329

   Completed iteration 5, pert 1 (MCC.Element1 = 0.760245431567)
   Completed iteration 5, pert 2 (MCC.Element2 = 0.788294042924)

DC Iteration 6; Nominal Pass
   Variables:  MCC.Element1 = 0.759781464755, MCC.Element2 = 0.788113772638
   Goals and achieved values:
      geoSat.EarthMJ2000Eq.INC  Desired: 2  Achieved: 1.99999919152  Variance: 8.08480441705e-07
      geoSat.RMAG  Desired: 42195  Achieved: 42195.010066  Variance: -0.0100659927921

   Completed iteration 6, pert 1 (MCC.Element1 = 0.759881464755)
   Completed iteration 6, pert 2 (MCC.Element2 = 0.788213772638)

DC Iteration 7; Nominal Pass
   Variables:  MCC.Element1 = 0.75978134961, MCC.Element2 = 0.788113687412
   Goals and achieved values:
      geoSat.EarthMJ2000Eq.INC  Desired: 2  Achieved: 1.99999999998  Variance: 2.19251283795e-11
      geoSat.RMAG  Desired: 42195  Achieved: 42195.0000008  Variance: -8.36393155623e-07


*** Targeting Completed in 7 iterations.
*** The Targeter converged!
Final Variable values:
   MCC.Element1 = 0.75978134961
   MCC.Element2 = 0.788113687412

********************************************************
*** 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: 57242.5935766  Variance: -15075.6935766

   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: 52144.5234866  Variance: -9977.62348664

   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: 47995.5748022  Variance: -5828.67480224

   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: 44557.5941035  Variance: -2390.69410347

   Completed iteration 4, pert 1 (MOI.Element1 = -0.3999)

DC Iteration 5; Nominal Pass
   Variables:  MOI.Element1 = -0.476084013834
   Goals and achieved values:
      geoSat.Earth.SMA  Desired: 42166.9  Achieved: 42314.8122254  Variance: -147.912225384

   Completed iteration 5, pert 1 (MOI.Element1 = -0.475984013834)

DC Iteration 6; Nominal Pass
   Variables:  MOI.Element1 = -0.481432602668
   Goals and achieved values:
      geoSat.Earth.SMA  Desired: 42166.9  Achieved: 42167.5548271  Variance: -0.65482708146

   Completed iteration 6, pert 1 (MOI.Element1 = -0.481332602668)

DC Iteration 7; Nominal Pass
   Variables:  MOI.Element1 = -0.481456488769
   Goals and achieved values:
      geoSat.Earth.SMA  Desired: 42166.9  Achieved: 42166.9000659  Variance: -6.59372017253e-05


*** Targeting Completed in 7 iterations.
*** The Targeter converged!
Final Variable values:
   MOI.Element1 = -0.481456488769

Mission run completed.
===> Total Run Time: 1.718 seconds

========================================


*** GMAT Integration test (Console version) successful! ***

Moderator is deleting core engine...
Test Summary: | Pass  Total  Time
GMAT          |    1      1  3.0s
     Testing GMAT tests passed 

Testing completed after 11.15s

PkgEval succeeded after 56.39s