I just committed a fix for the drag modelling issue that was first seen in the 2/4 build. We should see the % passed back above 99% in Monday's build.
- DJC On 2/6/2015 5:14 AM, [email protected] wrote: > ----------------------------------------------------------------- > Summary > ----------------------------------------------------------------- > System configuration: GS580W-GMAT-T4/Win7-64/GMAT-32/M2013a/VS2010 > Tested build: 2015-02-05 > Regression build: 2015-02-04 > > Total number of scripts: 12048 (+129 deferred) > Percent Passed: 98.93% > New issues: 2 > Output changes: 2 > New truth failures: 0 > New crashes: 0 > New script errors: 0 > New comparator errors: 0 > Fixed issues: 1 > Total issues: 129 > > Test system warnings: 11 > New deferred issues: 5 > Fixed deferred issues: 1 > Total deferred issues: 120 > > Run Time: 14 hours, 06 minutes, 04 seconds > > ----------------------------------------------------------------- > New Issues > ----------------------------------------------------------------- > New truth failures: > None > > Output changes (but still pass): > Ephem_GMAT_Code500_60sec > Ephem_GMAT_Code500_TimeInteractions > > Output changes (but still fail): > None > > New crashes/hangs/etc.: > None > > New script errors: > None > > New comparator errors: > None > > ----------------------------------------------------------------- > Fixed Issues > ----------------------------------------------------------------- > Fixed truth failures: > None > > Fixed crashes/hangs/etc.: > Math_Validation_Non-AllowedLHS_2 > > Fixed script errors: > None > > Fixed comparator errors: > None > > ----------------------------------------------------------------- > All Known Issues > ----------------------------------------------------------------- > Crashes/hangs/etc.: > None > > Script errors: > All_in_One_STEREO > BatchEstimator_InversionAlgorithm_2 > BatchEstimator_InversionAlgorithm_3 > BatchEstimator_InversionAlgorithm > BatchEstimator_Nominal_Geosynchronous_RangeDoppler > BatchEstimator_Nominal_Heliocentric_RangeDoppler > BatchEstimator_Nominal_L1_Range > BatchEstimator_Nominal_L2_Range > BatchEstimator_Nominal_Lunar_RangeDoppler > BatchEstimator_OLSEInitialRMSSigma_Doppler > BatchEstimator_OLSEInitialRMSSigma_Range > BatchEstimator_Propagator_Simulate_Earth8x8 > BatchEstimator_Propagator_Simulate_EarthFull > BatchEstimator_Propagator_Simulate_EarthPtMass_Drag > BatchEstimator_Propagator_Simulate_EarthPtMass_SRP_Drag > BatchEstimator_Propagator_Simulate_EarthPtMass_SRP > BatchEstimator_Propagator_Simulate_EarthPtMass > BatchEstimator_Propagator_Simulate_Sun_EM_AllPlanets_SRP_GR > BatchEstimator_Propagator_Simulate_Sun_EM_AllPlanets > BatchEstimator_Propagator_Simulate_Sun_EM_GR > BatchEstimator_Propagator_Simulate_Sun_EM > BatchEstimator_Propagator_Simulate_Sun_SRP > BatchEstimator_Propagator_Simulate_Sun > BatchEstimator_Propagator > BatchEstimator_ReportStyle_Concise > BatchEstimator_ReportStyle_Debug > BatchEstimator_ReportStyle_Normal > BatchEstimator_ReportStyle_Verbose > Estimate_LEO_PointMass_USNTwoWayRange_LightTimeOnly_NonPerturbedIC > Estimate_LEO_PointMass_USNTwoWayRange_LightTimeOnly_PerturbedIC > GS_Nav_DeepSpace_DSN_Media > Old_All_in_One_STEREO > Old_All_in_One > > Old_Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC_Ramp > > Old_Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC > Old_Estimate_LEO_PointMass_DSNTwoWayDoppler_LightTimeOnly_NonPerturbedIC > > Old_Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC_Ramp > > Old_Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC > Old_Estimate_LEO_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC > Old_Simulate_DeepSpace_DSNTwoWayDoppler_LightTimeOnly_RampTable > Old_Simulate_DeepSpace_DSNTwoWayRange_LT_GR_Transponder_RampTable > Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_GR_RampTable > Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable_2 > Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable > Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly > Old_Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Ramp > Old_Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Zero_Ramp > Old_Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly > Old_Simulate_LEO_DSNTwoWayRange_LightTimeOnly_RampTable > Old_Simulate_LEO_DSNTwoWayRange_LightTimeOnly > ScriptEvent_SmokeTests_Events_Eclipse_Simple > Simulate_DeepSpace_DSNTwoWayRange_LT_GR_Transponder_RampTable > Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_GR_RampTable > Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable_2 > Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly > TrkFile_Sim_DSN_DeepSpace_Range_LTO > TrkFile_Sim_DSN_LEO_Doppler_LTO > > Comparator errors: > Events_EclipseLocator_Simple (truth) > > Truth failures: > Ballistic_and_Mass_Case01_GTO [pos err 29.4814, tol 0.0025] > Ballistic_and_Mass_Case01_LEO [pos err 1.46818, tol 0.001] > Ballistic_and_Mass_Case01_LEO_Cmd [pos err 1.46818, tol 0.001] > Ballistic_and_Mass_Case02_GTO [pos err 43.2551, tol 0.0025] > Ballistic_and_Mass_Case02_LEO [pos err 2.15892, tol 0.001] > Ballistic_and_Mass_Case03_GTO [pos err 27.1626, tol 0.0025] > Ballistic_and_Mass_Case03_LEO [pos err 1.35026, tol 0.001] > Ballistic_and_Mass_Case04_GTO [pos err 1.23245, tol 0.0025] > Ballistic_and_Mass_Case04_LEO [pos err 0.121647, tol 0.001] > BatchEstimator_AddSolveFor_CartesianState [#1 failed] > BatchEstimator_AddSolveFor_CartesianState_DopplerBias [#1 failed] > BatchEstimator_AddSolveFor_CartesianState_DopplerBias2 [#1 failed] > BatchEstimator_AddSolveFor_CartesianState_DopplerBias3 [#1 failed] > BatchEstimator_AddSolveFor_CartesianState_RangeBias [#1 failed] > BatchEstimator_AddSolveFor_CartesianState_RangeBias2 [#1 failed] > BatchEstimator_AddSolveFor_CartesianState_RangeBias2_DopplerBias2 [#1 > failed] > BatchEstimator_AddSolveFor_CartesianState_RangeBias3 [#1 failed] > BatchEstimator_AddSolveFor_CartesianState_RangeBias3_DopplerBias3 [#1 > failed] > BatchEstimator_AddSolveFor_CartesianState_RangeBias_DopplerBias [#1 > failed] > BatchEstimator_InversionAlgorithm_NotEnoughData [ptrn 1,2 failed] > BatchEstimator_InversionAlgorithm_NotEnoughData_2 [ptrn 1,2 failed] > BatchEstimator_InversionAlgorithm_NotEnoughData_3 [ptrn 1,2 failed] > BatchEstimator_InversionAlgorithm_Singular [#1 failed] > BatchEstimator_InversionAlgorithm_Singular_2 [#1 failed] > BatchEstimator_InversionAlgorithm_Singular_3 [#1 failed] > BatchEstimator_MaxConsecutiveDivergences [ptrn 1,2 failed] > BatchEstimator_Measurements [#1 failed] > BatchEstimator_Measurements2 [#1 failed] > BatchEstimator_Measurements3 [#1 failed] > BatchEstimator_OLSE_NoDataEdited_AllIterations [#1 failed] > BatchEstimator_OLSE_NoDataEdited_FirstIteration [#1 failed] > BatchEstimator_OLSEAdditiveConstant_Doppler [#1 failed] > BatchEstimator_OLSEAdditiveConstant_Range [#1 failed] > BatchEstimator_OLSEMultiplicativeConstant_Doppler [#1 failed] > BatchEstimator_OLSEMultiplicativeConstant_Range [#1 failed] > BatchEstimator_Validation_AddSolveFor [#1 failed] > BatchEstimator_Validation_Measurements [#1 failed] > BatchEstimator_Validation_Mode [#1 failed] > BatchEstimator_Validation_ReportFile [#1 failed] > EphemPropagator_Origin_Earth_HST_5MinStepSize [pos err 0.517881, tol > 0.01] > EphemPropagator_Origin_Earth_HST_TestExtraStep [pos err 0.515198, tol > 0.01] > EphemPropagator_PropAssigmentToNewPropThenProp [pos err 0.517881, tol > 0.01] > EphemPropagator_PropDifferentSpacecraft [pos err 0.454003, tol 1e-07] > EphemPropagator_SatAssigmentToNewSatThenProp [pos err 0.517881, tol > 0.01] [GMT-3434] > EphemPropagator_StartEpoch_A1Gregorian [pos err 81.8951, tol 0.001] > EphemPropagator_StartEpoch_A1ModJulian [pos err 81.8952, tol 0.001] > EphemPropagator_StartEpoch_FromSpacecraft [pos err 81.8952, tol 0.001] > EphemPropagator_StartEpoch_TAIGregorian [pos err 81.8952, tol 0.001] > EphemPropagator_StartEpoch_TAIModJulian [pos err 81.8952, tol 0.001] > EphemPropagator_StartEpoch_TDBGregorian [pos err 81.8954, tol 0.001] > EphemPropagator_StartEpoch_TDBModJulian [pos err 81.8952, tol 0.001] > EphemPropagator_StartEpoch_TTGregorian [pos err 81.8952, tol 0.001] > EphemPropagator_StartEpoch_TTModJulian [pos err 81.8952, tol 0.001] > EphemPropagator_StartEpoch_UTCGregorian [pos err 81.8952, tol 0.001] > EphemPropagator_StartEpoch_UTCModJulian [pos err 81.8952, tol 0.001] > EphemPropagator_StepSize_1day [pos err 0.504113, tol 0.001] > EphemPropagator_StepSize_1day_ForLoop [pos err 0.504113, tol 0.001] > EphemPropagator_StepSize_1hour [pos err 0.492245, tol 0.001] > EphemPropagator_StepSize_1hour_ForLoop [pos err 0.492245, tol 0.001] > EphemPropagator_StepSize_2minutes [pos err 0.491893, tol 0.001] > EphemPropagator_StepSize_2minutes_ForLoop [pos err 0.491893, tol 0.001] > GMAT_ISS_Earth_0_JR_ModifiedFluxAndGeoMag [pos err 9.35943, tol 0.005] > GMAT_ISS_Earth_0_MSISE86_ModifiedFluxAndGeoMag [pos err 7.34676, tol > 0.002] > GMAT_ISS_Earth_0_MSISE90_ModifiedFluxAndGeoMag [pos err 7.39054, tol > 0.002] > GMAT_ISS_Earth_0_NRLMSISE00_ModifiedFluxAndGeoMag [pos err 7.30125, tol > 0.002] > GMAT_Mars1_Mars_0_MarsGRAM2005_0_NonDefaultF107 [pos err 0.0296918, tol > 0.0003] > GMAT_UserMoon-Titan_AllPlanets_SRP_AboutAsteroid [pos err 5569.14, tol > 0.002] > GMAT_UserMoon-Titan_AllPlanets_SRP_AboutComet [pos err 5569.14, tol > 0.002] > ScriptEvent_SmokeTests_Ballistic_and_Mass_Case04_LEO [pos err 0.121647, > tol 0.001] > ScriptLanguage_Validation_FilePaths_3 [no error or exception] > TargeterNesting [max diff 2.26405e-07 > tol 1e-07] > > ----------------------------------------------------------------- > New Issues (Deferred) > ----------------------------------------------------------------- > New truth failures (deferred): > None > > Output changes (but still pass) (deferred): > Ephem_GMAT_Code500_InterpolationOrder [GMT-4075, GMT-4112] > > Output changes (but still fail) (deferred): > Ephem_GMAT_Code500_ACE_OpsPrototype_v13 [pos err 1.36904, tol 1] > [GMT-4112] > > EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection > [pos err 15.2522, tol 1e-12] [GMT-4077] > > EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect > [pos err 14.1473, tol 1e-12] [GMT-4077] > EphemStressTests_SPK_Integrator_Code500_60Sec_ForwardDirection [pos err > 0.000427977, tol 1e-12] [GMT-4112] > > New crashes/hangs/etc. (deferred): > None > > New script errors (deferred): > None > > New comparator errors (deferred): > None > > ----------------------------------------------------------------- > Fixed Issues (Deferred) > ----------------------------------------------------------------- > Fixed truth failures (deferred): > None > > Fixed crashes/hangs/etc. (deferred): > Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455] > > Fixed script errors (deferred): > None > > Fixed comparator errors (deferred): > None > > ----------------------------------------------------------------- > All Known Issues (Deferred) > ----------------------------------------------------------------- > Crashes/hangs/etc. (deferred): > None > > Script errors (deferred): > All_in_One > > Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC_Ramp > Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC > Estimate_LEO_4x4_USNTwoWayRange_LightTimeOnly_NonPerturbedIC > Estimate_LEO_4x4_USNTwoWayRange_LightTimeOnly_PerturbedIC > Estimate_LEO_PointMass_DSNTwoWayDoppler_LightTimeOnly_NonPerturbedIC > > Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC_Ramp > > Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC > Estimate_LEO_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC > Ex_GmatFunction [GMT-3604] > Ex_Integrators > GMATFunction_ArrayIO > GMATFunction_EarthFixedPropFun_Periapsis > GMATFunction_EarthFixedPropFun > GMATFunction_FunInFun_Global > GMATFunction_FunInFun > GMATFunction_GlobalSC > GMATFunction_LiteralInput > GMATFunction_MJ2000EcPropFun_Apoapsis > GMATFunction_MJ2000EcProp > GMATFunction_MJ2000EqPropFun_Apoapsis > GMATFunction_MJ2000EqProp > GMATFunction_NoFunOutput > GMATFunction_NoIO_EditSC > GMATFunction_NoInput > GMATFunction_PassAndPropSC > GMATFunction_PassSC_NoFunOutput > GMATFunction_PlotFun > GMATFunction_Recursive > GMATFunction_SCIO_wprop > GMATFunction_SCIO > GMATFunction_SearchFunPath > GMATFunction_StringIO > GMATFunction_TwoFunOneFile > GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_BS > > GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Max_Reduction_BS > > GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Minimum_Reduction_BS > GMAT_LEO_PropSynchronization_BS > GMAT_LunarTran_PropSynchronization_BS > GMAT_LunarTransfer_AllPlanets_DE421_BS > GMAT_MarsTransfer_4_BS > GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS > Integrator_BS_InitialStep > Integrator_GEO_BS_2Body > Integrator_ISS_BS_2Body > Integrator_LEO_BS_Accuracy > Integrator_LEO_BS_ErrorControl > Integrator_Max_Step_BS > Math_Math_GmatFunction > Math_Shadowed_Builtins [GMT-3043] > STM_GMAT_BLSTR > Save_Barycenter > Save_DifferentialCorrector > Save_FiniteBurn > Save_Formation > Save_GroundStation_Cartesian > Save_GroundStation_Spherical > Save_ImpulsiveBurn_EarthFixed_Decrement_Tank1 > Save_ImpulsiveBurn_EarthFixed_Decrement_~Tank > Save_ImpulsiveBurn_EarthFixed_~Decrement > Save_ImpulsiveBurn_Local_Decrement_Tank1 > Save_ImpulsiveBurn_Local_Decrement_~Tank > Save_ImpulsiveBurn_Local_~Decrement > Save_LibrationPoint > Save_SQP > Save_Simulator > Save_Thruster_EarthFixed_Decrement_NoTank > Save_Thruster_EarthFixed_Decrement_Tank1 > Save_Thruster_EarthFixed_NoDecrement > Save_Thruster_Local_Decrement_NoTank > Save_Thruster_Local_Decrement_Tank1 > Save_Thruster_Local_NoDecrement > ScriptEvent_SmokeTests_Save_GroundStation_Spherical > ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522] > Simulate_DeepSpace_DSNTwoWayDoppler_LightTimeOnly_RampTable > Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable > Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Ramp > Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Zero_Ramp > Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly > Simulate_LEO_DSNTwoWayRange_LightTimeOnly_RampTable > Simulate_LEO_DSNTwoWayRange_LightTimeOnly > Simulate_LEO_USNTwoWayRange_LightTime-Bias > Simulate_LEO_USNTwoWayRange_LightTimeOnly > Target_DC_Command_GMATFunction > Target_DC_Command_Save > Thruster_FBurn_Earth_ScA_ThrusterB_CS2_TankA_BS > Thruster_FBurn_Earth_ScA_ThrusterB_CS3_TankL_BS > Thruster_FBurn_Earth_ScA_ThrusterB_CS3_TankL_Max_Reduction_BS > Thruster_FBurn_Earth_ScA_ThrusterB_CS3_TankL_Minimum_Reduction_BS > > Comparator errors (deferred): > None > > Truth failures (deferred): > Achieve_Validation_LHS_Field [ptrn 1 failed] [GMT-3687] > Achieve_Validation_RHS_Field [no error or exception] [GMT-3687] > BatchEstimator_AbsoluteTol [ptrn 1 failed] > BatchEstimator_MaximumIterations [ptrn 1,2 failed] > BatchEstimator_RelativeTol [ptrn 1 failed] > Ephem_GMAT_Code500_ACE_OpsPrototype_v13 [pos err 1.36904, tol 1] > [GMT-4112] > > Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_1.eph > [pos err 0.0177967, tol 0.002] [GMT-4075, GMT-4112] > > Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_3.eph > [pos err 0.0463976, tol 0.002] [GMT-4075, GMT-4112] > Ephem_GMAT_Code500_StepSize/Ephem_GMAT_Code500_StepSize_1.eph [pos err > 305.165, tol 0.002] [GMT-4112] > > EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection > [pos err 15.2522, tol 1e-12] [GMT-4077] > > EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection > [pos err 9.57664, tol 1e-12] [GMT-4077] > > EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect > [pos err 14.1473, tol 1e-12] [GMT-4077] > > EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection > [pos err 0.000224514, tol 1e-12] [GMT-4112] > EphemStressTests_PD78_ABM_Prop_Code500_60Sec_Step_ForwardDirection [pos > err 21.5627, tol 1e-12] [GMT-4112] > EphemStressTests_SPK_Integrator_Code500_60Sec_ForwardDirection [pos err > 0.000427977, tol 1e-12] [GMT-4112] > Epoch_LeapSecond_G2MJD [max mjd diff 1.000259s > tol 0.001000s] [2561] > Epoch_LeapSecond_In [max mjd diff 1.000111s > tol 0.001000s] [2561] > Epoch_LeapSecond_Out [max mjd diff 1.000146s > tol 0.001000s] [2561] > Formation_Validation_MissingComma [no error or exception] [GMT-3672] > GMAT_ISS_Earth_JGM2_0_0_NutationUpdateInterval [pos err 0.00081427, tol > 1e-06] [GMT-2567] > Math_Inf [GMAT: 53 lines, Truth: 69 lines] [GMT-3195] > Minimize_Validation_Field [no warn or err] [GMT-3687] > Nonlinear_Validation_LHS_Field [no warn or err] [GMT-3687] > Nonlinear_Validation_RHS_Field [no warn or err] [GMT-3687] > ScriptLanguage_Comments_AfterControlFlow [] [GMT-3332] > ScriptLanguage_LineContinuation_BeginningOfLine [] [GMT-3756] > ScriptLanguage_LiteralArrays_String [] [GMT-3680] > ScriptLanguage_ReferenceArrays_ForceModel_7 [] [GMT-3541] > ScriptLanguage_Validation_Semicolons_1 [no error or exception] > [GMT-3545] > String_AssignNumericParam [] [GMT-2888] > Vary_Validation_RHS_Field [no error or exception] [GMT-3687] > > ----------------------------------------------------------------- > Test System Warnings > ----------------------------------------------------------------- > Passing tests tagged with bugs: > (To fix, remove bug ID from Bugs key in .tc file) > Comet_Validation_OrientationEpoch_3 [GMT-3252] > CoordSysTest_Luna_MJ2000Eq_To_ICRF [GMT-3227] > CoordinateSystem_Validation_Axes_4 [GMT-3155] > Formation_Validation_PropFormSatInTwoProps [GMT-3581] > GMAT_GEO_EarthSunMoon_0_0_0_Relativity [3405] > GMAT_GEO_EarthSun_0_0_0_Relativity [3405] > GMAT_ISS_EarthSunMoon_0_0_0_Relativity [3405] > GMAT_ISS_EarthSunMoon_0_0_0_Relativity_Cmd [3405] > GMAT_ISS_EarthSun_0_0_0_Relativity [3405] > SpacePointParams_CelestialBody_EpochOutput [3939] > Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455] > > > ------------------------------------------------------------------------------ > Dive into the World of Parallel Programming. The Go Parallel Website, > sponsored by Intel and developed in partnership with Slashdot Media, is your > hub for all things parallel software development, from weekly thought > leadership blogs to news, videos, case studies, tutorials and more. Take a > look and join the conversation now. http://goparallel.sourceforge.net/ > _______________________________________________ > Gmat-buildtest mailing list > [email protected] > https://lists.sourceforge.net/lists/listinfo/gmat-buildtest > > > -- Darrel J. Conway, Ph.D. Thinking Systems, Inc. Senior Scientist and CEO 6441 N Camino Libby Phone: (623) 298-4530 Tucson, AZ 85718 FAX: (520) 232-2533 www.thinksysinc.com Cell: (520) 425-3626 [email protected] ------------------------------------------------------------------------------ Dive into the World of Parallel Programming. The Go Parallel Website, sponsored by Intel and developed in partnership with Slashdot Media, is your hub for all things parallel software development, from weekly thought leadership blogs to news, videos, case studies, tutorials and more. Take a look and join the conversation now. http://goparallel.sourceforge.net/ _______________________________________________ Gmat-buildtest mailing list [email protected] https://lists.sourceforge.net/lists/listinfo/gmat-buildtest
