(cd run_OMSimulator-cs-cvode && /home/hudson/saved_omc/OMSimulator/install/bin/OMSimulator --resultFile=../ClaRa_dev_ClaRa.Components.TurboMachines.Compressors.Check.Test_MassFlow_VIGVControlled_OMSimulator-cs-cvode_res.mat --stripRoot --tempDir=temp_ClaRa_dev_ClaRa_Components_TurboMachines_Compressors_Check_Test_MassFlow_VIGVControlled_OMSimulator-cs-cvode_fmu --startTime=0 --stopTime=30 --stepSize=0.012 --mode=cs --timeout=240 --tolerance=1e-06 ../ClaRa_dev_ClaRa_Components_TurboMachines_Compressors_Check_Test_MassFlow_VIGVControlled_OMSimulator-cs-cvode.fmu) LOG_SOLVER | info | CVODE linear multistep method CV_BDF LOG_SOLVER | info | CVODE maximum integration order CV_ITER_NEWTON LOG_SOLVER | info | CVODE use equidistant time grid YES LOG_SOLVER | info | CVODE Using relative error tolerance 1.000000e-06 LOG_SOLVER | info | CVODE Using dense internal linear solver SUNLinSol_Dense. LOG_SOLVER | info | CVODE Use internal dense numeric jacobian method. LOG_SOLVER | info | CVODE uses internal root finding method NO LOG_SOLVER | info | CVODE maximum absolut step size 0 LOG_SOLVER | info | CVODE initial step size is set automatically LOG_SOLVER | info | CVODE maximum integration order 5 LOG_SOLVER | info | CVODE maximum number of nonlinear convergence failures permitted during one step 10 LOG_SOLVER | info | CVODE BDF stability limit detection algorithm OFF info: *** FMU Simulation Info *** - model : ClaRa.Components.TurboMachines.Compressors.Check.Test_MassFlow_VIGVControlled (co-simulation) - fmiVersion: 2.0 - startTime : 0.000000 - stopTime : 30.000000 - tolerance : 1e-06 - stepSize : 0.012 LOG_ASSERT | debug | /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelicaLibraryTesting/ClaRa_dev_ClaRa.Components.TurboMachines.Compressors.Check.Test_MassFlow_VIGVControlled/499.fmutmp/sources/ClaRa_dev_ClaRa_Components_TurboMachines_Compressors_Check_Test_MassFlow_VIGVControlled_02nls.c:187: Invalid root: (-nan)^(3.49526) LOG_STDOUT | warning | Non-Linear Solver try to handle a problem with a called assert. LOG_ASSERT | debug | /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelicaLibraryTesting/ClaRa_dev_ClaRa.Components.TurboMachines.Compressors.Check.Test_MassFlow_VIGVControlled/499.fmutmp/sources/ClaRa_dev_ClaRa_Components_TurboMachines_Compressors_Check_Test_MassFlow_VIGVControlled_02nls.c:187: Invalid root: (-nan)^(3.49526) LOG_ASSERT | debug | /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelicaLibraryTesting/ClaRa_dev_ClaRa.Components.TurboMachines.Compressors.Check.Test_MassFlow_VIGVControlled/499.fmutmp/sources/ClaRa_dev_ClaRa_Components_TurboMachines_Compressors_Check_Test_MassFlow_VIGVControlled_02nls.c:177: Invalid root: (-53.0732)^(3.49526) LOG_STDOUT | warning | While solving non-linear system an assertion failed during initialization. | | | | | The non-linear solver tries to solve the problem that could take some time. | | | | | It could help to provide better start-values for the iteration variables. | | | | | For more information simulate with -lv LOG_NLS_V LOG_ASSERT | debug | /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelicaLibraryTesting/ClaRa_dev_ClaRa.Components.TurboMachines.Compressors.Check.Test_MassFlow_VIGVControlled/499.fmutmp/sources/ClaRa_dev_ClaRa_Components_TurboMachines_Compressors_Check_Test_MassFlow_VIGVControlled_02nls.c:187: Invalid root: (-nan)^(3.49526) LOG_ASSERT | debug | /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelicaLibraryTesting/ClaRa_dev_ClaRa.Components.TurboMachines.Compressors.Check.Test_MassFlow_VIGVControlled/499.fmutmp/sources/ClaRa_dev_ClaRa_Components_TurboMachines_Compressors_Check_Test_MassFlow_VIGVControlled_02nls.c:187: Invalid root: (-nan)^(3.49526) LOG_ASSERT | error | [/home/hudson/saved_omc/libraries/.openmodelica/libraries/ClaRa 1.9.0-main/Components/TurboMachines/Compressors/CompressorGas_L1_stageStacked.mo:1007:6-1008:98:writable] | | | | The following assertion has been violated during initialization at time 0.000000 | | | | ((GasFanAdvanced.phi_rel_st[1] > GasFanAdvanced.phi_surge_rel_st[1])) --> "************StackedCompressorStages: Surge line exceeded in last stage************" error: [fmi2logger] [fmi2Error] Test_MassFlow_VIGVControlled/logFmi2Call: fmi2ExitInitializationMode: terminated by an assertion. error: [initialize] fmi2_exitInitializationMode failed for FMU "Test_MassFlow_VIGVControlled.root.Test_MassFlow_VIGVControlled" error: [initialize] Initialization of system "Test_MassFlow_VIGVControlled.root" failed Traceback (most recent call last): File "", line 198, in _run_module_as_main File "", line 88, in _run_code File "/home/hudson/saved_omc/OMSimulator/install/lib/x86_64-linux-gnu/OMSimulator/__main__.py", line 38, in sys.exit(main()) ~~~~^^ File "/home/hudson/saved_omc/OMSimulator/install/lib/x86_64-linux-gnu/OMSimulator/cli.py", line 309, in main handler(args.model, args) ~~~~~~~^^^^^^^^^^^^^^^^^^ File "/home/hudson/saved_omc/OMSimulator/install/lib/x86_64-linux-gnu/OMSimulator/cli.py", line 175, in _runFMU fmu.initialize() ~~~~~~~~~~~~~~^^ File "/home/hudson/saved_omc/OMSimulator/install/lib/x86_64-linux-gnu/OMSimulator/fmu.py", line 887, in initialize raise RuntimeError(f"Failed to initialize model: {status}") RuntimeError: Failed to initialize model: Status.error info: 0 warnings info: 3 errors