Running: ./testmodel.py --libraries=/home/hudson/saved_omc/libraries/.openmodelica/libraries --ompython_omhome=/usr Buildings_13_Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance.conf.json loadFile("/home/hudson/saved_omc/libraries/.openmodelica/libraries/ModelicaServices 4.1.0+maint.om/package.mo", uses=false) [Timeout 180] "Notification: Performance of loadFile(/home/hudson/saved_omc/libraries/.openmodelica/libraries/ModelicaServices 4.1.0+maint.om/package.mo): time 0.002447/0.002447, allocations: 80.88 kB / 21.56 MB, free: 2.93 MB / 18.57 MB " [Timeout remaining time 180] loadFile("/home/hudson/saved_omc/libraries/.openmodelica/libraries/Complex 4.1.0+maint.om/package.mo", uses=false) [Timeout 180] "Notification: Performance of loadFile(/home/hudson/saved_omc/libraries/.openmodelica/libraries/Complex 4.1.0+maint.om/package.mo): time 0.002354/0.002354, allocations: 170.1 kB / 24.97 MB, free: 9.199 MB / 18.57 MB " [Timeout remaining time 180] loadFile("/home/hudson/saved_omc/libraries/.openmodelica/libraries/Modelica 4.1.0+maint.om/package.mo", uses=false) [Timeout 180] "Notification: Performance of loadFile(/home/hudson/saved_omc/libraries/.openmodelica/libraries/Modelica 4.1.0+maint.om/package.mo): time 1.755/1.755, allocations: 177.1 MB / 205.4 MB, free: 5.461 MB / 186.7 MB " [Timeout remaining time 178] loadFile("/home/hudson/saved_omc/libraries/.openmodelica/libraries/Buildings 13.0.2-maint.13.x/package.mo", uses=false) [Timeout 180] "Notification: Performance of loadFile(/home/hudson/saved_omc/libraries/.openmodelica/libraries/Buildings 13.0.2-maint.13.x/package.mo): time 3.316/3.316, allocations: 389.5 MB / 0.6361 GB, free: 12.31 MB / 0.6042 GB " [Timeout remaining time 176] Using package Buildings with version 13.0.2 (/home/hudson/saved_omc/libraries/.openmodelica/libraries/Buildings 13.0.2-maint.13.x/package.mo) Using package Modelica with version 4.1.0 (/home/hudson/saved_omc/libraries/.openmodelica/libraries/Modelica 4.1.0+maint.om/package.mo) Using package Complex with version 4.1.0 (/home/hudson/saved_omc/libraries/.openmodelica/libraries/Complex 4.1.0+maint.om/package.mo) Using package ModelicaServices with version 4.1.0 (/home/hudson/saved_omc/libraries/.openmodelica/libraries/ModelicaServices 4.1.0+maint.om/package.mo) Running command: translateModel(Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance,tolerance=1e-06,outputFormat="empty",numberOfIntervals=2500,variableFilter="",fileNamePrefix="Buildings_13_Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance") translateModel(Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance,tolerance=1e-06,outputFormat="empty",numberOfIntervals=2500,variableFilter="",fileNamePrefix="Buildings_13_Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance") [Timeout 300] OMC exited with status 139 while running: translateModel(Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance,tolerance=1e-06,outputFormat="empty",numberOfIntervals=2500,variableFilter="",fileNamePrefix="Buildings_13_Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance") Created ZeroMQ Server. Dumped server port in file: /tmp/openmodelica.hudson.port.1c205dd094404b098b470be4286ff4d5[stateselection] (0) Forced states by StateSelect.ALWAYS: *********************************************************** [stateselection] (3) Natural states before index reduction: ************************************************************* [STAT] (1) Real air.vol.U (start = Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance.air.vol.dynBal.Medium.specificInternalEnergy(Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance.Medium.setState_pTX(air.vol.dynBal.p_start, air.vol.dynBal.T_start, air.vol.dynBal.X_start[1:1])) * air.vol.dynBal.fluidVolume * air.vol.dynBal.rho_start + air.vol.dynBal.CSen * ((-273.15) + air.vol.dynBal.T_start)) [STAT] (1) protected Real air.vol.dynBal.m (start = air.vol.V * air.vol.rho_start, min = 0.0, StateSelect = prefer) [STAT] (1) Real[1] air.vol.Xi = air.vol.Xi (start = air.vol.dynBal.X_start[1:1], min = {max(0.0, ({0.0})[$i749]) for $i749 in 1:1}, max = {min(1.0, ({1.0})[$i750]) for $i750 in 1:1}) [stateselection] State Order: ******************************* (air.vol.dynBal.m --d/dt--> air.vol.dynBal.mb_flow) [stateselection] (6) State Derivatives Created by Differentiation ******************************************************************* [DDER] (1) Real $DER.air.vol.dynBal.medium.d (StateSelect = avoid) [DDER] (1) Real[1] $DER.air.vol.ports.p (StateSelect = avoid) [DDER] (1) Real $DER.$FUN_1.p (StateSelect = avoid) [DDER] (1) Real $DER.$FUN_2 (StateSelect = avoid) [DDER] (1) Real[1] $DER.air.ports.p (StateSelect = avoid) [DDER] (1) Real[1] $DER.boundary.ports.p (StateSelect = avoid) [stateselection] (7) Selected Dummy States ******************************************** [DSTA] (1) protected Real air.vol.dynBal.medium.d (start = 1.2 * (9.869232667160129e-6 * air.vol.dynBal.p_start), min = 0.0, max = 1184.3079200592153, nominal = 1.0) [DSTA] (1) Real[1] air.ports.p (start = {101325.0 for $f2 in 1:1}, min = {0.0 for $f4 in 1:1}, max = {1e8 for $f3 in 1:1}, nominal = {1e5 for $f1 in 1:1}) [DSTA] (1) Real $FUN_2 (start = Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance.air.vol.dynBal.Medium.density($FUN_1), min = 0.0, max = 1e5, nominal = 1.0) [DSTA] (1) Real[1] boundary.ports.p (start = {101325.0 for $f2 in 1:1}, min = {0.0 for $f4 in 1:1}, max = {1e8 for $f3 in 1:1}, nominal = {1e5 for $f1 in 1:1}) [DSTA] (1) Real[1] air.vol.ports.p (start = {101325.0 for $f2 in 1:1}, min = {max(({0.0})[$i747], 0.0) for $i747 in 1:1}, max = {min(({1e8})[$i748], 1e8) for $i748 in 1:1}, nominal = {1e5 for $f1 in 1:1}) [DSTA] (1) Real $FUN_1.p (start = 101325.0, min = 0.0, max = 1e8, nominal = 1e5) [DSTA] (1) protected Real air.vol.dynBal.m (start = air.vol.V * air.vol.rho_start, min = 0.0, StateSelect = prefer) Created State Start Equations (2): ************************************ [ARRY] (1) $START.air.vol.Xi = air.vol.dynBal.X_start[1:1]; ($RES_SRT_326) [SCAL] (1) $START.air.vol.U = Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance.air.vol.dynBal.Medium.specificInternalEnergy(Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance.Medium.setState_pTX(air.vol.dynBal.p_start, air.vol.dynBal.T_start, air.vol.dynBal.X_start[1:1])) * air.vol.dynBal.fluidVolume * air.vol.dynBal.rho_start + air.vol.dynBal.CSen * ((-273.15) + air.vol.dynBal.T_start); ($RES_SRT_325) Created Algebraic Start Equations (11): ***************************************** [SCAL] (1) $START.air.vol.dynBal.m = air.vol.V * air.vol.rho_start; ($RES_SRT_337) [ARRY] (2) $START.$FUN_19 = {air.vol.dynBal.X_start[1], 0.0}; ($RES_SRT_336) [SCAL] (1) $START.$FUN_13.p = (Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance.Medium.setState_pTX(boundary.p_in_internal, boundary.T_in_internal, boundary.X_in_internal)).p; ($RES_SRT_335) [SCAL] (1) $START.$FUN_13.T = (Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance.Medium.setState_pTX(boundary.p_in_internal, boundary.T_in_internal, boundary.X_in_internal)).T; ($RES_SRT_334) [SCAL] (1) $START.air.vol.hOut_internal = air.vol.dynBal.hStart; ($RES_SRT_333) [SCAL] (1) $START.air.vol.dynBal.medium.dT = (-273.15) + air.vol.dynBal.T_start; ($RES_SRT_332) [ARRY] (2) $START.air.vol.dynBal.medium.X = air.vol.dynBal.X_start; ($RES_SRT_331) [SCAL] (1) $START.air.vol.dynBal.medium.d = 1.2 * (9.869232667160129e-6 * air.vol.dynBal.p_start); ($RES_SRT_330) [ARRY] (1) $START.air.vol.dynBal.ports.h_outflow = {air.vol.dynBal.hStart}; ($RES_SRT_329) [ARRY] (1) $START.air.vol.mXi = air.vol.dynBal.rho_start * air.vol.dynBal.fluidVolume * air.vol.dynBal.X_start[1:1]; ($RES_SRT_328) [SCAL] (1) $START.air.vol.T = air.vol.T_start; ($RES_SRT_327) Created Secondary Parameter Binding Equations (23): ***************************************************** [ARRY] (7) air.surBou = surBou; ($RES_BND_382) [ARRY] (36) air.datConBou = datConBou; ($RES_BND_381) [ARRY] (36) air.datConPar = datConPar; ($RES_BND_380) [ARRY] (85) air.datConExtWin = datConExtWin; ($RES_BND_379) [ARRY] (36) air.datConExt = datConExt; ($RES_BND_378) [SCAL] (1) qRadGai_flow.y = qRadGai_flow.k; ($RES_BND_377) [SCAL] (1) qConGai_flow.y = qConGai_flow.k; ($RES_BND_376) [SCAL] (1) qLatGai_flow.y = qLatGai_flow.k; ($RES_BND_375) [ARRY] (1) air.convConExt.is_floor = {$FUN_28 < 1e-9 and air.convConExt[1].cosTil < 0.0}; ($RES_BND_370) [ARRY] (1) air.convConExt.is_ceiling = {$FUN_28 < 1e-9 and air.convConExt[1].cosTil > 0.0}; ($RES_BND_369) [ARRY] (1) air.convConExt.sinTil = {$FUN_27}; ($RES_BND_368) [ARRY] (1) air.convConExt.cosTil = {$FUN_26}; ($RES_BND_367) [ARRY] (1) air.convConExt.til = {air.datConExt[1].til}; ($RES_BND_366) [SCAL] (1) air.convConExt[1].hFixed = air.hFixed; ($RES_BND_365) [ARRY] (1) air.convConExt.A = {air.AConExt[1]}; ($RES_BND_364) [SCAL] (1) air.vol.dynBal.rho_start = $FUN_23; ($RES_BND_361) [ARRY] (1) air.ASurBou = air.surBou.A; ($RES_BND_350) [ARRY] (1) air.AConBou = air.datConBou.A; ($RES_BND_349) [ARRY] (1) air.AConPar = air.datConPar.A; ($RES_BND_348) [ARRY] (1) air.AConExtWinFra = air.datConExtWin.fFra .* air.datConExtWin.AWin; ($RES_BND_347) [ARRY] (1) air.AConExtWinGla = (1.0 .- air.datConExtWin.fFra) .* air.datConExtWin.AWin; ($RES_BND_346) [ARRY] (1) air.AConExtWinOpa = air.datConExtWin.AOpa; ($RES_BND_345) [ARRY] (1) air.AConExt = air.datConExt.A; ($RES_BND_344) Created Primary Parameter Binding Equations (27): *************************************************** BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: protected Real boundary.p_in_internal = boundary.p ### Equation: [SCAL] (1) boundary.p_in_internal = boundary.p; ($RES_BND_374) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: protected Real boundary.T_in_internal = boundary.T ### Equation: [SCAL] (1) boundary.T_in_internal = boundary.T; ($RES_BND_373) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 2) -------------------------------------------------------------------- ### Variable: protected Real[2] boundary.X_in_internal = boundary.X ### Equation: [ARRY] (2) boundary.X_in_internal = boundary.X; ($RES_BND_372) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: protected Real[1] boundary.Xi_in_internal = boundary.X[{1}] ### Equation: [ARRY] (1) boundary.Xi_in_internal = boundary.X[{1}]; ($RES_BND_371) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: final parameter Real air.vol.V = air.V ### Equation: [SCAL] (1) air.vol.V = air.V; ($RES_BND_356) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: final parameter Real air.vol.m_flow_nominal = air.m_flow_nominal ### Equation: [SCAL] (1) air.vol.m_flow_nominal = air.m_flow_nominal; ($RES_BND_354) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 2) -------------------------------------------------------------------- ### Variable: final parameter Real[2] air.vol.X_start = air.X_start ### Equation: [ARRY] (2) air.vol.X_start = air.X_start; ($RES_BND_353) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: final parameter Real air.vol.T_start = air.T_start ### Equation: [SCAL] (1) air.vol.T_start = air.T_start; ($RES_BND_352) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: final parameter Real air.vol.p_start = air.p_start ### Equation: [SCAL] (1) air.vol.p_start = air.p_start; ($RES_BND_351) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: final parameter Integer[1] air.dummyCon.nSta = {air.dummyCon.material[1].nSta} ### Equation: [ARRY] (1) air.dummyCon.nSta = {air.dummyCon.material[1].nSta}; ($RES_BND_343) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: final parameter Real air.dummyCon.R = air.dummyCon.material[1].R ### Equation: [SCAL] (1) air.dummyCon.R = air.dummyCon.material[1].R; ($RES_BND_342) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: final parameter Real[1] datConExtWin.AWin = {datConExtWin[1].wWin * datConExtWin[1].hWin} ### Equation: [ARRY] (1) datConExtWin.AWin = {datConExtWin[1].wWin * datConExtWin[1].hWin}; ($RES_BND_338) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: Real $FUN_21 ### Equation: [SCAL] (1) $FUN_21 = abs(air.m_flow_nominal); ($RES_AUX_220) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 4) -------------------------------------------------------------------- ### Variable: protected final parameter Medium.ThermodynamicState air.vol.state_start = Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance.Medium.setState_pTX(air.vol.p_start, air.vol.T_start, air.vol.X_start[1:1]) ### Equation: [RECD] (4) air.vol.state_start = Buildings.ThermalZones.Detailed.BaseClasses.Examples.MixedAirHeatMassBalance.Medium.setState_pTX(air.vol.p_start, air.vol.T_start, air.vol.X_start[1:1]); ($RES_BND_383) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: protected final parameter Real air.vol.dynBal.fluidVolume = air.vol.V ### Equation: [SCAL] (1) air.vol.dynBal.fluidVolume = air.vol.V; ($RES_BND_360) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 2) -------------------------------------------------------------------- ### Variable: protected final parameter Real[2] air.vol.dynBal.X_start = air.vol.X_start ### Equation: [ARRY] (2) air.vol.dynBal.X_start = air.vol.X_start; ($RES_BND_359) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: protected final parameter Real air.vol.dynBal.T_start = air.vol.T_start ### Equation: [SCAL] (1) air.vol.dynBal.T_start = air.vol.T_start; ($RES_BND_358) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: protected final parameter Real air.vol.dynBal.p_start = air.vol.p_start ### Equation: [SCAL] (1) air.vol.dynBal.p_start = air.vol.p_start; ($RES_BND_357) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: parameter Real air.vol.m_flow_small = 1e-4 * $FUN_21 ### Equation: [SCAL] (1) air.vol.m_flow_small = 1e-4 * $FUN_21; ($RES_BND_355) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: final parameter Real[1] datConExtWin.AFra = {datConExtWin[1].AWin * datConExtWin[1].fFra} ### Equation: [ARRY] (1) datConExtWin.AFra = {datConExtWin[1].AWin * datConExtWin[1].fFra}; ($RES_BND_340) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: final parameter Real[1] datConExtWin.AOpa = {datConExtWin[1].A - datConExtWin[1].AWin} ### Equation: [ARRY] (1) datConExtWin.AOpa = {datConExtWin[1].A - datConExtWin[1].AWin}; ($RES_BND_339) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: Real $FUN_24 ### Equation: [SCAL] (1) $FUN_24 = 1006.0 * ((-273.15) + air.vol.dynBal.T_start) * (1.0 - air.vol.dynBal.X_start[1]) + (2.5010145e6 + 1860.0 * ((-273.15) + air.vol.dynBal.T_start)) * air.vol.dynBal.X_start[1]; ($RES_AUX_217) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: Real $FUN_25 ### Equation: [SCAL] (1) $FUN_25 = 1.1843079200592153e-5 * air.vol.state_start.p; ($RES_AUX_216) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 2) -------------------------------------------------------------------- ### Variable: Real[2] $START.$FUN_19 ### Equation: [ARRY] (2) $START.$FUN_19 = {air.vol.dynBal.X_start[1], 0.0}; ($RES_SRT_336) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: protected parameter Real air.vol.rho_start = $FUN_25 ### Equation: [SCAL] (1) air.vol.rho_start = $FUN_25; ($RES_BND_363) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: protected parameter Real air.vol.dynBal.hStart = $FUN_24 ### Equation: [SCAL] (1) air.vol.dynBal.hStart = $FUN_24; ($RES_BND_362) BLOCK: Single Strong Component (status = Solve.EXPLICIT, size = 1) -------------------------------------------------------------------- ### Variable: final parameter Real[1] datConExtWin.AGla = {datConExtWin[1].AWin - datConExtWin[1].AFra} ### Equation: [ARRY] (1) datConExtWin.AGla = {datConExtWin[1].AWin - datConExtWin[1].AFra}; ($RES_BND_341) ############################## Balance Initialization ############################## Not underdetermined. ********************** Stage 1 overdetermined. (1) Unmatched equations: ************************** [SCAL] (1) 101325.0 * (0.8333333333333334 * air.vol.dynBal.medium.d) = air.vol.dynBal.p_start; ($RES_SIM_3) Created Start Equations for balancing the Initialization (0): *************************************************************** Limited backtrace at point of segmentation fault /usr/lib/x86_64-linux-gnu/libc.so.6(+0x45cb0) [0x7e7fd3e24cb0] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1) [0x7e7fd5ecca81] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1af) [0x7e7fd5eccc2f] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1af) [0x7e7fd5eccc2f] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1af) [0x7e7fd5eccc2f] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1ec) [0x7e7fd5eccc6c] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1af) [0x7e7fd5eccc2f] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1af) [0x7e7fd5eccc2f] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1af) [0x7e7fd5eccc2f] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1ec) [0x7e7fd5eccc6c] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1af) [0x7e7fd5eccc2f] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1af) [0x7e7fd5eccc2f] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1af) [0x7e7fd5eccc2f] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1ec) [0x7e7fd5eccc6c] /var/lib/jenkins/ws/OpenModelicaLibraryTestingWork/OpenModelica/OMCompiler/build/bin/../lib/x86_64-linux-gnu/omc/libOpenModelicaRuntimeMMC.so(valueCompare+0x1af) [0x7e7fd5eccc2f] Segmentation fault (core dumped) [Calling os._exit(0), Time elapsed: 14.312973731197417]