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libtool: install: /usr/bin/install -c .libs/libISSMMatlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/libISSMMatlab.la
libtool: install: /usr/bin/install -c .libs/libISSMApi_matlab.dylib /Users/jenkins/workspace/macOS-Intel-Examples/lib/libISSMApi_matlab.dylib
libtool: install: /usr/bin/install -c .libs/libISSMApi_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/libISSMApi_matlab.la
libtool: install: /usr/bin/install -c .libs/BamgConvertMesh_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/BamgConvertMesh_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/BamgConvertMesh_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/BamgConvertMesh_matlab.la
libtool: install: /usr/bin/install -c .libs/BamgMesher_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/BamgMesher_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/BamgMesher_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/BamgMesher_matlab.la
libtool: install: /usr/bin/install -c .libs/BamgTriangulate_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/BamgTriangulate_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/BamgTriangulate_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/BamgTriangulate_matlab.la
libtool: install: /usr/bin/install -c .libs/ContourToMesh_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/ContourToMesh_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/ContourToMesh_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/ContourToMesh_matlab.la
libtool: install: /usr/bin/install -c .libs/ContourToNodes_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/ContourToNodes_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/ContourToNodes_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/ContourToNodes_matlab.la
libtool: install: /usr/bin/install -c .libs/DistanceToMaskBoundary_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/DistanceToMaskBoundary_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/DistanceToMaskBoundary_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/DistanceToMaskBoundary_matlab.la
libtool: install: /usr/bin/install -c .libs/ElementConnectivity_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/ElementConnectivity_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/ElementConnectivity_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/ElementConnectivity_matlab.la
libtool: install: /usr/bin/install -c .libs/ExpSimplify_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/ExpSimplify_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/ExpSimplify_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/ExpSimplify_matlab.la
libtool: install: /usr/bin/install -c .libs/ExpToLevelSet_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/ExpToLevelSet_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/ExpToLevelSet_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/ExpToLevelSet_matlab.la
libtool: install: /usr/bin/install -c .libs/InterpFromGrid_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromGrid_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/InterpFromGrid_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromGrid_matlab.la
libtool: install: /usr/bin/install -c .libs/InterpFromGridToMesh_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromGridToMesh_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/InterpFromGridToMesh_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromGridToMesh_matlab.la
libtool: install: /usr/bin/install -c .libs/InterpFromMesh2d_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromMesh2d_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/InterpFromMesh2d_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromMesh2d_matlab.la
libtool: install: /usr/bin/install -c .libs/InterpFromMeshToGrid_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromMeshToGrid_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/InterpFromMeshToGrid_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromMeshToGrid_matlab.la
libtool: install: /usr/bin/install -c .libs/InterpFromMeshToMesh2d_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromMeshToMesh2d_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/InterpFromMeshToMesh2d_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromMeshToMesh2d_matlab.la
libtool: install: /usr/bin/install -c .libs/InterpFromMeshToMesh3d_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromMeshToMesh3d_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/InterpFromMeshToMesh3d_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/InterpFromMeshToMesh3d_matlab.la
libtool: install: /usr/bin/install -c .libs/IssmConfig_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/IssmConfig_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/IssmConfig_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/IssmConfig_matlab.la
libtool: install: /usr/bin/install -c .libs/MeshPartition_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/MeshPartition_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/MeshPartition_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/MeshPartition_matlab.la
libtool: install: /usr/bin/install -c .libs/MeshProfileIntersection_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/MeshProfileIntersection_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/MeshProfileIntersection_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/MeshProfileIntersection_matlab.la
libtool: install: /usr/bin/install -c .libs/NodeConnectivity_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/NodeConnectivity_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/NodeConnectivity_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/NodeConnectivity_matlab.la
libtool: install: /usr/bin/install -c .libs/PointCloudFindNeighbors_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/PointCloudFindNeighbors_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/PointCloudFindNeighbors_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/PointCloudFindNeighbors_matlab.la
libtool: install: /usr/bin/install -c .libs/ProcessRifts_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/ProcessRifts_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/ProcessRifts_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/ProcessRifts_matlab.la
libtool: install: /usr/bin/install -c .libs/PropagateFlagsFromConnectivity_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/PropagateFlagsFromConnectivity_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/PropagateFlagsFromConnectivity_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/PropagateFlagsFromConnectivity_matlab.la
libtool: install: /usr/bin/install -c .libs/Triangle_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/Triangle_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/Triangle_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/Triangle_matlab.la
libtool: install: /usr/bin/install -c .libs/Chaco_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/Chaco_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/Chaco_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/Chaco_matlab.la
libtool: install: /usr/bin/install -c .libs/Kriging_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/Kriging_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/Kriging_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/Kriging_matlab.la
libtool: install: /usr/bin/install -c .libs/CoordTransform_matlab.mexmaci64 /Users/jenkins/workspace/macOS-Intel-Examples/lib/CoordTransform_matlab.mexmaci64
libtool: install: /usr/bin/install -c .libs/CoordTransform_matlab.lai /Users/jenkins/workspace/macOS-Intel-Examples/lib/CoordTransform_matlab.la
make[4]: Nothing to be done for `install-data-am'.
make[4]: Nothing to be done for `install-exec-am'.
make[4]: Nothing to be done for `install-data-am'.
make[3]: Nothing to be done for `install-exec-am'.
make[3]: Nothing to be done for `install-data-am'.
make[2]: Nothing to be done for `install-exec-am'.
make[2]: Nothing to be done for `install-data-am'.
Testing example: AMR
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Coarse mesh
Construction of a mesh from a given geometry
Step 2: Parameterization
boundary conditions for stressbalance model: spc set as zero
no smb.mass_balance specified: values set as zero
no basalforcings.groundedice_melting_rate specified: values set as zero
no basalforcings.floatingice_melting_rate specified: values set as zero
no balancethickness.thickening_rate specified: values set as zero
no thermal boundary conditions created: no observed temperature found
Step 3: Solve!
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/mismip-06-30-2026-05-13-28-32501/mismip.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
call computational core:
[92miteration 1/500 time [yr]: 1.00[m (time step: 1.00)
computing smb
computing new velocity
computing basal mass balance
computing mass transport
[0] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[0] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
[1] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[1] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
loading results from cluster
[Warning: Could not copy
/Users/jenkins/workspace/macOS-Intel-Examples//execution/mismip-06-30-2026-05-13-28-32501//mismip.outbin]
[> In issmscpin (line 22)
In generic/Download (line 328)
In loadresultsfromcluster (line 45)
In solve (line 210)
In runme (line 65)]
Error using loadresultsfromdisk
=========================================================================
Binary file mismip.outbin not found
This typically results from an error encountered during the simulation
Please check for error messages above or in the outlog
=========================================================================
Error in loadresultsfromcluster (line 48)
md=loadresultsfromdisk(md,[md.miscellaneous.name '.outbin']);
Error in solve (line 210)
md=loadresultsfromcluster(md);
Error in runme (line 65)
md=solve(md,'Transient');FAILURE
Directory contains datasets only; no example to run.
Testing example: EsaGRACE
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Global mesh creation
Info : Running 'gmsh -2 sphere.geo' [Gmsh 4.14.2-git-0cebcd9, 1 node, max. 1 thread]
Info : Started on Tue Jun 30 05:14:04 2026
Info : Reading 'sphere.geo'...
Info : Done reading 'sphere.geo'
Info : Meshing 1D...
Info : [ 0%] Meshing curve 1 (Circle)
Info : [ 10%] Meshing curve 2 (Circle)
Info : [ 20%] Meshing curve 3 (Circle)
Info : [ 30%] Meshing curve 4 (Circle)
Info : [ 40%] Meshing curve 5 (Circle)
Info : [ 50%] Meshing curve 6 (Circle)
Info : [ 60%] Meshing curve 7 (Circle)
Info : [ 60%] Meshing curve 8 (Circle)
Info : [ 70%] Meshing curve 9 (Circle)
Info : [ 80%] Meshing curve 10 (Circle)
Info : [ 90%] Meshing curve 11 (Circle)
Info : [100%] Meshing curve 12 (Circle)
Info : Done meshing 1D (Wall 0.00470433s, CPU 0.00232s)
Info : Meshing 2D...
Info : [ 0%] Meshing surface 14 (Surface, MeshAdapt)
Info : [ 20%] Meshing surface 16 (Surface, MeshAdapt)
Info : [ 30%] Meshing surface 18 (Surface, MeshAdapt)
Info : [ 40%] Meshing surface 20 (Surface, MeshAdapt)
Info : [ 60%] Meshing surface 22 (Surface, MeshAdapt)
Info : [ 70%] Meshing surface 24 (Surface, MeshAdapt)
Info : [ 80%] Meshing surface 26 (Surface, MeshAdapt)
Info : [ 90%] Meshing surface 28 (Surface, MeshAdapt)
Info : Done meshing 2D (Wall 87.4357s, CPU 33.8863s)
Info : 7669 nodes 15747 elements
Info : Writing 'sphere.msh'...
Info : Done writing 'sphere.msh'
Info : Stopped on Tue Jun 30 05:15:31 2026 (From start: Wall 87.7579s, CPU 34.0148s)
gmtmask: num vertices 7668
gmtmask: done
2026-06-30 05:15:48.630 MATLAB[34841:203470488] CoreText note: Client requested name ".SFNS-Regular", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
2026-06-30 05:15:48.631 MATLAB[34841:203470488] CoreText note: Set a breakpoint on CTFontLogSystemFontNameRequest to debug.
2026-06-30 05:15:48.639 MATLAB[34841:203470488] CoreText note: Client requested name ".SFNS-Bold", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
2026-06-30 05:15:48.652 MATLAB[34841:203470488] CoreText note: Client requested name ".SFNS-Regular", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
2026-06-30 05:15:48.653 MATLAB[34841:203470488] CoreText note: Client requested name ".SFNS-Bold", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
Step 2: Define loads in meters of ice height equivalent
1 of 1 months done!
Step 3: Parameterization
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In runme (line 65)]
Step 4: Solve Esa solver
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/EsaGRACE-06-30-2026-05-16-02-34841/EsaGRACE.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
starting model processor
creating datasets for analysis EsaAnalysis
updating elements and materials for control parameters
updating elements and materials for uncertainty quantification
creating output definitions
done with model processor
Processing finite element model of analysis EsaAnalysis:
toolkits Options set for analysis: EsaAnalysis
configuring element and loads
Configuring elements...
Configuring loads...
Configuring materials...
Configuring inputs...
detecting active vertices
resolving node constraints
creating nodal degrees of freedom
Renumbering degrees of freedom
call computational core:
computing elastic adjustment
toolkits Options set for analysis: EsaAnalysis
computing elastic geodetic core
write lock file:
FemModel initialization elapsed time: 0.401278
Total Core solution elapsed time: 22.7696
Linear solver elapsed time: 0 (0%)
Total elapsed time: 0 hrs 0 min 23 sec
WARNING! There are options you set that were not used!
WARNING! could be spelling mistake, etc!
There are 7 unused database options. They are:
Option left: name:-ksp_type value: preonly source: code
Option left: name:-mat_mumps_icntl_14 value: 120 source: code
Option left: name:-mat_mumps_icntl_28 value: 2 source: code
Option left: name:-mat_mumps_icntl_29 value: 2 source: code
Option left: name:-mat_type value: mpiaij source: code
Option left: name:-pc_factor_mat_solver_type value: mumps source: code
Option left: name:-pc_type value: lu source: code
loading results from cluster
Step 5: Plot solutions
SUCCESS
Testing example: EsaWahr
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Mesh creation
2026-06-30 05:17:12.442 MATLAB[45557:203491975] CoreText note: Client requested name ".SFNS-Regular", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
2026-06-30 05:17:12.442 MATLAB[45557:203491975] CoreText note: Set a breakpoint on CTFontLogSystemFontNameRequest to debug.
2026-06-30 05:17:12.455 MATLAB[45557:203491975] CoreText note: Client requested name ".SFNS-Bold", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
2026-06-30 05:17:12.473 MATLAB[45557:203491975] CoreText note: Client requested name ".SFNS-Regular", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
2026-06-30 05:17:12.473 MATLAB[45557:203491975] CoreText note: Client requested name ".SFNS-Bold", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
Step 2: Anisotropic mesh creation
Anisotropic mesh adaptation
WARNING: mesh present but no geometry found. Reconstructing...
new number of triangles = 4207
Step 3: Define loads
Step 4: Parameterization
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In runme (line 73)]
Step 5: Solve Esa solver
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/EsaWahr-06-30-2026-05-17-19-45557/EsaWahr.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
starting model processor
creating datasets for analysis EsaAnalysis
updating elements and materials for control parameters
updating elements and materials for uncertainty quantification
creating output definitions
done with model processor
Processing finite element model of analysis EsaAnalysis:
toolkits Options set for analysis: EsaAnalysis
configuring element and loads
Configuring elements...
Configuring loads...
Configuring materials...
Configuring inputs...
detecting active vertices
resolving node constraints
creating nodal degrees of freedom
Renumbering degrees of freedom
call computational core:
computing elastic adjustment
toolkits Options set for analysis: EsaAnalysis
computing elastic geodetic core
write lock file:
FemModel initialization elapsed time: 0.18698
Total Core solution elapsed time: 0.832978
Linear solver elapsed time: 0 (0%)
Total elapsed time: 0 hrs 0 min 1 sec
WARNING! There are options you set that were not used!
WARNING! could be spelling mistake, etc!
There are 7 unused database options. They are:
Option left: name:-ksp_type value: preonly source: code
Option left: name:-mat_mumps_icntl_14 value: 120 source: code
Option left: name:-mat_mumps_icntl_28 value: 2 source: code
Option left: name:-mat_mumps_icntl_29 value: 2 source: code
Option left: name:-mat_type value: mpiaij source: code
Option left: name:-pc_factor_mat_solver_type value: mumps source: code
Option left: name:-pc_type value: lu source: code
loading results from cluster
Step 6: Plot solutions
Step 7: Compare results against Wahr semi-analytic solutions
SUCCESS
Directory contains functions only; no example to run.
Testing example: Greenland
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Mesh creation
Anisotropic mesh adaptation
WARNING: mesh present but no geometry found. Reconstructing...
new number of triangles = 6345
2026-06-30 05:17:48.210 MATLAB[57804:203498043] CoreText note: Client requested name ".SFNS-Regular", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
2026-06-30 05:17:48.210 MATLAB[57804:203498043] CoreText note: Set a breakpoint on CTFontLogSystemFontNameRequest to debug.
2026-06-30 05:17:48.215 MATLAB[57804:203498043] CoreText note: Client requested name ".SFNS-Bold", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
2026-06-30 05:17:48.223 MATLAB[57804:203498043] CoreText note: Client requested name ".SFNS-Regular", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
2026-06-30 05:17:48.223 MATLAB[57804:203498043] CoreText note: Client requested name ".SFNS-Bold", it will get Times-Roman rather than the intended font. All system UI font access should be through proper APIs such as CTFontCreateUIFontForLanguage() or +[NSFont systemFontOfSize:].
Step 2: Parameterization
Loading SeaRISE data from NetCDF
Interpolating surface and bedrock
Constructing thickness
Interpolating velocities
Interpolating temperatures
Interpolating surface mass balance
Construct basal friction parameters
Construct ice rheological properties
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In TemporaryParameterFile57804 (line 54)
In parameterize (line 29)
In runme (line 41)]
Set other boundary conditions
Set geothermal heat flux
Set Pressure
Single point constraints
Step 3: Control method friction
checking model consistency
INFO: the outlog will look better if only md.verbose.control is turned on
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-17-52-57804/SeaRISEgreenland.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
call computational core:
preparing initial solution
x | Cost function f(x) | List of contributions
====================== step 1/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 59172.79 | 7092.887 52079.9 6.085212e-32
x = 1 | f(x) = 50954.87 | 3600.244 47354.58 0.04587451
====================== step 2/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 50953.45 | 3598.809 47354.6 0.04587451
x = 1 | f(x) = 44978.74 | 2137.679 42840.82 0.2370654
====================== step 3/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 44987.02 | 2146.197 42840.58 0.2370654
x = 1 | f(x) = 44425.8 | 2044.873 42380.66 0.2722667
====================== step 4/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 44432.36 | 2051.851 42380.24 0.2722667
x = 1 | f(x) = 42775.97 | 1747.394 41028.16 0.4148691
====================== step 5/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 42783.98 | 1756.726 41026.84 0.4148691
x = 1 | f(x) = 41876.1 | 1659.336 40216.23 0.5302616
====================== step 6/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 41885.98 | 1670.347 40215.1 0.5302616
x = 1 | f(x) = 40869.39 | 1561.173 39307.52 0.6932322
====================== step 7/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 40870.91 | 1563.273 39306.95 0.6932322
x = 1 | f(x) = 39697.76 | 1338.256 38358.58 0.9236775
====================== step 8/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 39697.43 | 1338.655 38357.85 0.9236775
x = 1 | f(x) = 39040.22 | 1208.675 37830.47 1.071791
====================== step 9/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 39039.49 | 1208.558 37829.86 1.071791
x = 1 | f(x) = 38556.09 | 1126.764 37428.13 1.191478
====================== step 10/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 38552.98 | 1124.507 37427.28 1.191478
x = 1 | f(x) = 38121.56 | 1092.495 37027.74 1.3288
====================== step 11/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 38122.77 | 1094.958 37026.49 1.3288
x = 1 | f(x) = 37729.41 | 1149.628 36578.29 1.493932
====================== step 12/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37740.46 | 1159.142 36579.82 1.493932
x = 1 | f(x) = 37487.92 | 1087.186 36399.14 1.592633
x = 0.381966 | f(x) = 37611.19 | 1112.303 36497.36 1.529775
x = 0.618034 | f(x) = 37561.1 | 1101.089 36458.46 1.55338
x = 0.763932 | f(x) = 37530.94 | 1093.798 36435.58 1.568476
x = 0.854102 | f(x) = 37512.65 | 1089.499 36421.58 1.577683
x = 0.90983 | f(x) = 37501.45 | 1086.979 36412.88 1.583344
====================== step 13/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37484.86 | 1084.592 36398.67 1.592633
x = 1 | f(x) = 37022.46 | 1018.285 36002.41 1.768007
====================== step 14/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37030.9 | 1026.085 36003.05 1.768007
x = 1 | f(x) = 36814.89 | 1058.135 35754.9 1.859438
x = 0.381966 | f(x) = 36898.13 | 989.5907 35906.74 1.799676
x = 0.618034 | f(x) = 36853.98 | 1003.884 35848.28 1.821225
x = 0.763932 | f(x) = 36838.62 | 1025.038 35811.75 1.835325
x = 0.937069 | f(x) = 36824.08 | 1052.478 35769.75 1.852853
x = 0.870937 | f(x) = 36839.21 | 1051.966 35785.4 1.846056
====================== step 15/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36824.8 | 1068.389 35754.55 1.859438
x = 1 | f(x) = 36559.07 | 954.0377 35603.09 1.936544
x = 0.381966 | f(x) = 36711.5 | 1017.403 35692.21 1.887487
x = 0.618034 | f(x) = 36653.71 | 995.7569 35656.05 1.905392
x = 0.763932 | f(x) = 36614.76 | 978.0481 35634.8 1.916939
x = 0.854102 | f(x) = 36589.85 | 965.9689 35621.95 1.92432
x = 0.90983 | f(x) = 36574.06 | 958.1749 35613.95 1.928974
====================== step 16/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36552.27 | 948.6767 35601.65 1.936544
x = 1 | f(x) = 36368.74 | 909.4905 35457.24 2.009954
x = 0.381966 | f(x) = 36450.66 | 912.2196 35536.48 1.964688
x = 0.618034 | f(x) = 36415.28 | 905.8741 35507.42 1.981913
x = 0.763932 | f(x) = 36394.68 | 904.2792 35488.41 1.992565
x = 0.854102 | f(x) = 36384.31 | 906.0028 35476.31 1.999281
x = 0.90983 | f(x) = 36379.73 | 908.9319 35468.79 2.003357
====================== step 17/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36373.34 | 914.7542 35456.58 2.009954
x = 1 | f(x) = 36229.12 | 957.6674 35269.34 2.111313
x = 0.381966 | f(x) = 36289.06 | 905.1848 35381.82 2.046875
x = 0.618034 | f(x) = 36257.86 | 916.5034 35339.28 2.070593
x = 0.763932 | f(x) = 36247.49 | 932.6872 35312.72 2.085785
x = 0.913021 | f(x) = 36239.38 | 951.6387 35285.64 2.101794
x = 0.856074 | f(x) = 36249.62 | 951.977 35295.55 2.095621
====================== step 18/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36238.23 | 966.1893 35269.93 2.111313
x = 1 | f(x) = 36005.81 | 893.306 35110.31 2.18899
x = 0.381966 | f(x) = 36142.54 | 929.6447 35210.76 2.139784
x = 0.618034 | f(x) = 36093.23 | 916.1558 35174.92 2.158128
x = 0.763932 | f(x) = 36058.58 | 905.5225 35150.89 2.16975
x = 0.854102 | f(x) = 36036.9 | 898.7214 35136 2.177043
x = 0.90983 | f(x) = 36023.73 | 894.6151 35126.93 2.18159
====================== step 19/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36005.22 | 890.2107 35112.82 2.18899
x = 1 | f(x) = 35868.42 | 869.9581 34996.18 2.287732
x = 0.381966 | f(x) = 35911.39 | 860.1821 35048.98 2.225541
x = 0.618034 | f(x) = 35893.04 | 858.0691 35032.72 2.249067
x = 0.763932 | f(x) = 35881.94 | 859.7353 35019.94 2.263658
x = 0.854102 | f(x) = 35877.04 | 863.763 35011.01 2.272799
x = 0.90983 | f(x) = 35875.47 | 868.0771 35005.11 2.278502
====================== step 20/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35873.35 | 875.6681 34995.4 2.287732
x = 1 | f(x) = 35723.35 | 910.5513 34810.43 2.374027
x = 0.381966 | f(x) = 35789.66 | 860.5594 34926.79 2.319061
x = 0.618034 | f(x) = 35757.04 | 868.789 34885.91 2.339232
x = 0.763932 | f(x) = 35744.03 | 883.7317 34857.95 2.352231
x = 0.854102 | f(x) = 35739.94 | 897.5494 34840.03 2.360435
x = 0.930997 | f(x) = 35737.52 | 910.28 34824.87 2.367548
====================== step 21/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35735.84 | 922.2347 34811.23 2.374027
x = 1 | f(x) = 35602.51 | 870.7784 34729.3 2.423398
x = 0.381966 | f(x) = 35668.82 | 880.0971 34786.33 2.391628
x = 0.618034 | f(x) = 35644.9 | 872.7159 34769.79 2.403223
x = 0.763932 | f(x) = 35629.08 | 870.0702 34756.6 2.410606
x = 0.854102 | f(x) = 35618.25 | 868.4465 34747.39 2.415368
x = 0.90983 | f(x) = 35610.89 | 867.4925 34740.98 2.418388
====================== step 22/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35599.85 | 867.5045 34729.92 2.423398
x = 1 | f(x) = 35435.33 | 841.7746 34591.04 2.515761
x = 0.381966 | f(x) = 35503.09 | 830.83 34669.8 2.457304
x = 0.618034 | f(x) = 35463.09 | 825.8312 34634.77 2.479098
x = 0.763932 | f(x) = 35440.81 | 828.0732 34610.24 2.492898
x = 0.854102 | f(x) = 35432.56 | 834.5397 34595.51 2.501553
x = 0.90983 | f(x) = 35438.35 | 841.9242 34593.91 2.50695
====================== step 23/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35439.26 | 840.4865 34596.27 2.501553
x = 1 | f(x) = 35377.76 | 827.9225 34547.29 2.55107
x = 0.381966 | f(x) = 35416.76 | 819.8319 34594.41 2.518729
x = 0.618034 | f(x) = 35399.79 | 819.4099 34577.85 2.530419
x = 0.763932 | f(x) = 35393.8 | 822.2266 34569.04 2.538053
x = 0.944313 | f(x) = 35386.99 | 828.3334 34556.1 2.547926
x = 0.875413 | f(x) = 35393.31 | 829.0398 34561.73 2.544098
====================== step 24/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35389.05 | 833.3283 34553.17 2.55107
x = 1 | f(x) = 35252.08 | 814.3328 34435.09 2.649675
x = 0.381966 | f(x) = 35317.08 | 812.978 34501.52 2.588143
x = 0.618034 | f(x) = 35288.37 | 809.7173 34476.04 2.611631
x = 0.763932 | f(x) = 35271.33 | 809.3561 34459.34 2.626304
x = 0.854102 | f(x) = 35263.63 | 811.1878 34449.81 2.635229
x = 0.90983 | f(x) = 35260.58 | 813.8445 34444.09 2.640723
====================== step 25/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35256.61 | 818.8748 34435.09 2.649675
x = 1 | f(x) = 35162.53 | 858.2923 34301.5 2.735676
x = 0.381966 | f(x) = 35180.62 | 812.9346 34365.01 2.680864
x = 0.618034 | f(x) = 35153.13 | 821.9691 34328.46 2.701321
x = 0.763932 | f(x) = 35158.4 | 837.054 34318.64 2.714146
x = 0.645763 | f(x) = 35167.63 | 833.394 34331.53 2.703727
x = 0.527864 | f(x) = 35170.22 | 824.2448 34343.28 2.693583
====================== step 26/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35160.91 | 827.091 34331.12 2.701321
x = 1 | f(x) = 35121.46 | 799.6831 34319.05 2.727669
x = 0.381966 | f(x) = 35148.31 | 811.7235 34333.88 2.710518
x = 0.618034 | f(x) = 35139.87 | 807.5893 34329.56 2.716727
x = 0.763932 | f(x) = 35133.07 | 803.7521 34326.59 2.720776
x = 0.854102 | f(x) = 35127.96 | 801.0169 34324.22 2.723359
x = 0.90983 | f(x) = 35124.32 | 799.2107 34322.38 2.724986
====================== step 27/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35118.96 | 797.3025 34318.93 2.727669
x = 1 | f(x) = 34992.01 | 809.2473 34179.93 2.832751
x = 0.381966 | f(x) = 35054.02 | 790.9422 34260.31 2.766228
x = 0.618034 | f(x) = 35029.18 | 793.4468 34232.94 2.790931
x = 0.763932 | f(x) = 35015.1 | 799.223 34213.07 2.806635
x = 0.854102 | f(x) = 35009.09 | 806.1057 34200.17 2.816507
x = 0.90983 | f(x) = 35007.38 | 812.598 34191.96 2.822672
====================== step 28/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35004.32 | 822.0413 34179.44 2.832751
x = 1 | f(x) = 34934.87 | 806.5674 34125.43 2.869513
x = 0.381966 | f(x) = 34947.17 | 786.7793 34157.54 2.846471
x = 0.618034 | f(x) = 34937.13 | 788.8927 34145.38 2.855048
x = 0.763932 | f(x) = 34935.7 | 795.0416 34137.8 2.860456
x = 0.748008 | f(x) = 34937.94 | 796.546 34138.54 2.859861
x = 0.854102 | f(x) = 34938.57 | 802.5726 34133.14 2.863862
====================== step 29/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 34941.3 | 812.7678 34125.66 2.869513
x = 1 | f(x) = 34824.78 | 779.576 34042.26 2.935698
x = 0.381966 | f(x) = 34880.03 | 788.1485 34088.99 2.894439
x = 0.618034 | f(x) = 34858.6 | 784.1171 34071.57 2.91002
x = 0.763932 | f(x) = 34843.88 | 780.8715 34060.09 2.919804
x = 0.854102 | f(x) = 34835.32 | 779.3894 34053.01 2.925896
x = 0.90983 | f(x) = 34830.74 | 779.0445 34048.76 2.929623
====================== step 30/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 34824.9 | 779.6846 34042.28 2.935698
x = 1 | f(x) = 34721.73 | 773.8226 33944.9 3.012811
x = 0.381966 | f(x) = 34777.78 | 771.9937 34002.82 2.964712
x = 0.618034 | f(x) = 34756.76 | 772.5218 33981.26 2.983082
x = 0.763932 | f(x) = 34743.45 | 772.8096 33967.65 2.994363
x = 0.854102 | f(x) = 34735.33 | 773.2066 33959.12 3.001402
x = 0.90983 | f(x) = 34730.47 | 773.6083 33953.86 3.005763
preparing final solution
computing new velocity
write lock file:
FemModel initialization elapsed time: 0.134429
Total Core solution elapsed time: 97.4304
Linear solver elapsed time: 58.3618 (60%)
Total elapsed time: 0 hrs 1 min 37 sec
loading results from cluster
Step 4: Transient run
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-19-39-57804/SeaRISEgreenland.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
Input updates from constant
Input updates from constant
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
call computational core:
Updating Mmes
[92miteration 1/100 time [yr]: 0.20[m (time step: 0.20)
computing smb
computing new velocity
Updating constraints and active domain of analysis StressbalanceAnalysis for time: 0.2
Get solution from inputs
Reduce vector from g to f set
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.05155e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 41.3709 > 1 %
Convergence criterion: norm(du)/norm(u) 63.1692 > 10 %
Convergence criterion: max(du) 0.000157031
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.08287e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 3.67351 > 1 %
Convergence criterion: norm(du)/norm(u) 7.15747 < 10 %
Convergence criterion: max(du) 8.86618e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.21945e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 1.10917 > 1 %
Convergence criterion: norm(du)/norm(u) 2.86495 < 10 %
Convergence criterion: max(du) 5.14918e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.01372e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 0.445157 < 1 %
Convergence criterion: norm(du)/norm(u) 1.23492 < 10 %
Convergence criterion: max(du) 2.12087e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
total number of iterations: 4
computing basal mass balance
computing mass transport
Updating constraints and active domain of analysis MasstransportAnalysis for time: 0.2
Allocating matrices
[1] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[1] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
(Kff stiffness matrix size: 3699 x 3699)
Assembling matrices
[0] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[0] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
loading results from cluster
[Warning: Could not copy
/Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-19-39-57804//SeaRISEgreenland.outbin]
[> In issmscpin (line 22)
In generic/Download (line 328)
In loadresultsfromcluster (line 45)
In solve (line 210)
In runme (line 111)]
Error using loadresultsfromdisk
=========================================================================
Binary file SeaRISEgreenland.outbin not found
This typically results from an error encountered during the simulation
Please check for error messages above or in the outlog
=========================================================================
Error in loadresultsfromcluster (line 48)
md=loadresultsfromdisk(md,[md.miscellaneous.name '.outbin']);
Error in solve (line 210)
md=loadresultsfromcluster(md);
Error in runme (line 111)
md=solve(md,'Transient');FAILURE
Not implemented yet!
+++ Removing old junit reports from: /Users/jenkins/workspace/macOS-Intel-Examples/nightlylog/results
+++ Running case: Example-AMR
+++ working dir: /Users/jenkins/workspace/macOS-Intel-Examples/nightlylog
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Coarse mesh
Construction of a mesh from a given geometry
Step 2: Parameterization
boundary conditions for stressbalance model: spc set as zero
no smb.mass_balance specified: values set as zero
no basalforcings.groundedice_melting_rate specified: values set as zero
no basalforcings.floatingice_melting_rate specified: values set as zero
no balancethickness.thickening_rate specified: values set as zero
no thermal boundary conditions created: no observed temperature found
Step 3: Solve!
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/mismip-06-30-2026-05-13-28-32501/mismip.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
call computational core:
iteration 1/500 time [yr]: 1.00 (time step: 1.00)
computing smb
computing new velocity
computing basal mass balance
computing mass transport
[0] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[0] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
[1] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[1] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
loading results from cluster
[Warning: Could not copy
/Users/jenkins/workspace/macOS-Intel-Examples//execution/mismip-06-30-2026-05-13-28-32501//mismip.outbin]
[> In issmscpin (line 22)
In generic/Download (line 328)
In loadresultsfromcluster (line 45)
In solve (line 210)
In runme (line 65)]
Error using loadresultsfromdisk
=========================================================================
Binary file mismip.outbin not found
This typically results from an error encountered during the simulation
Please check for error messages above or in the outlog
=========================================================================
Error in loadresultsfromcluster (line 48)
md=loadresultsfromdisk(md,d.miscellaneous.name '.outbin']);
Error in solve (line 210)
md=loadresultsfromcluster(md);
Error in runme (line 65)
md=solve(md,'Transient');FAILURE
+++ exit code: 0
+++ error: 0
+++ Running case: Example-AMR
+++ working dir: /Users/jenkins/workspace/macOS-Intel-Examples/nightlylog
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Coarse mesh
Construction of a mesh from a given geometry
Step 2: Parameterization
boundary conditions for stressbalance model: spc set as zero
no smb.mass_balance specified: values set as zero
no basalforcings.groundedice_melting_rate specified: values set as zero
no basalforcings.floatingice_melting_rate specified: values set as zero
no balancethickness.thickening_rate specified: values set as zero
no thermal boundary conditions created: no observed temperature found
Step 3: Solve!
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/mismip-06-30-2026-05-13-28-32501/mismip.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
call computational core:
iteration 1/500 time [yr]: 1.00 (time step: 1.00)
computing smb
computing new velocity
computing basal mass balance
computing mass transport
[0] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[0] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
[1] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[1] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
loading results from cluster
[Warning: Could not copy
/Users/jenkins/workspace/macOS-Intel-Examples//execution/mismip-06-30-2026-05-13-28-32501//mismip.outbin]
[> In issmscpin (line 22)
In generic/Download (line 328)
In loadresultsfromcluster (line 45)
In solve (line 210)
In runme (line 65)]
Error using loadresultsfromdisk
=========================================================================
Binary file mismip.outbin not found
This typically results from an error encountered during the simulation
Please check for error messages above or in the outlog
=========================================================================
Error in loadresultsfromcluster (line 48)
md=loadresultsfromdisk(md,d.miscellaneous.name '.outbin']);
Error in solve (line 210)
md=loadresultsfromcluster(md);
Error in runme (line 65)
md=solve(md,'Transient');FAILURE
+++ exit code: 0
+++ error: 1
+++ Running case: Example-EsaGRACE
+++ working dir: /Users/jenkins/workspace/macOS-Intel-Examples/nightlylog
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Global mesh creation
Info : Running 'gmsh -2 sphere.geo' [Gmsh 4.14.2-git-0cebcd9, 1 node, max. 1 thread]
Info : Started on Tue Jun 30 05:14:04 2026
Info : Reading 'sphere.geo'...
Info : Done reading 'sphere.geo'
Info : Meshing 1D...
Info : [ 0%] Meshing curve 1 (Circle)
Info : [ 10%] Meshing curve 2 (Circle)
Info : [ 20%] Meshing curve 3 (Circle)
Info : [ 30%] Meshing curve 4 (Circle)
Info : [ 40%] Meshing curve 5 (Circle)
Info : [ 50%] Meshing curve 6 (Circle)
Info : [ 60%] Meshing curve 7 (Circle)
Info : [ 60%] Meshing curve 8 (Circle)
Info : [ 70%] Meshing curve 9 (Circle)
Info : [ 80%] Meshing curve 10 (Circle)
Info : [ 90%] Meshing curve 11 (Circle)
Info : [100%] Meshing curve 12 (Circle)
Info : Done meshing 1D (Wall 0.00470433s, CPU 0.00232s)
Info : Meshing 2D...
Info : [ 0%] Meshing surface 14 (Surface, MeshAdapt)
Info : [ 20%] Meshing surface 16 (Surface, MeshAdapt)
Info : [ 30%] Meshing surface 18 (Surface, MeshAdapt)
Info : [ 40%] Meshing surface 20 (Surface, MeshAdapt)
Info : [ 60%] Meshing surface 22 (Surface, MeshAdapt)
Info : [ 70%] Meshing surface 24 (Surface, MeshAdapt)
Info : [ 80%] Meshing surface 26 (Surface, MeshAdapt)
Info : [ 90%] Meshing surface 28 (Surface, MeshAdapt)
Info : Done meshing 2D (Wall 87.4357s, CPU 33.8863s)
Info : 7669 nodes 15747 elements
Info : Writing 'sphere.msh'...
Info : Done writing 'sphere.msh'
Info : Stopped on Tue Jun 30 05:15:31 2026 (From start: Wall 87.7579s, CPU 34.0148s)
gmtmask: num vertices 7668
gmtmask: done
Step 2: Define loads in meters of ice height equivalent
1 of 1 months done!
Step 3: Parameterization
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In runme (line 65)]
Step 4: Solve Esa solver
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/EsaGRACE-06-30-2026-05-16-02-34841/EsaGRACE.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
starting model processor
creating datasets for analysis EsaAnalysis
updating elements and materials for control parameters
updating elements and materials for uncertainty quantification
creating output definitions
done with model processor
Processing finite element model of analysis EsaAnalysis:
toolkits Options set for analysis: EsaAnalysis
configuring element and loads
Configuring elements...
Configuring loads...
Configuring materials...
Configuring inputs...
detecting active vertices
resolving node constraints
creating nodal degrees of freedom
Renumbering degrees of freedom
call computational core:
computing elastic adjustment
toolkits Options set for analysis: EsaAnalysis
computing elastic geodetic core
write lock file:
FemModel initialization elapsed time: 0.401278
Total Core solution elapsed time: 22.7696
Linear solver elapsed time: 0 (0%)
Total elapsed time: 0 hrs 0 min 23 sec
WARNING! There are options you set that were not used!
WARNING! could be spelling mistake, etc!
There are 7 unused database options. They are:
Option left: name:-ksp_type value: preonly source: code
Option left: name:-mat_mumps_icntl_14 value: 120 source: code
Option left: name:-mat_mumps_icntl_28 value: 2 source: code
Option left: name:-mat_mumps_icntl_29 value: 2 source: code
Option left: name:-mat_type value: mpiaij source: code
Option left: name:-pc_factor_mat_solver_type value: mumps source: code
Option left: name:-pc_type value: lu source: code
loading results from cluster
Step 5: Plot solutions
SUCCESS
+++ exit code: 0
+++ error: 0
+++ Running case: Example-EsaGRACE
+++ working dir: /Users/jenkins/workspace/macOS-Intel-Examples/nightlylog
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Global mesh creation
Info : Running 'gmsh -2 sphere.geo' [Gmsh 4.14.2-git-0cebcd9, 1 node, max. 1 thread]
Info : Started on Tue Jun 30 05:14:04 2026
Info : Reading 'sphere.geo'...
Info : Done reading 'sphere.geo'
Info : Meshing 1D...
Info : [ 0%] Meshing curve 1 (Circle)
Info : [ 10%] Meshing curve 2 (Circle)
Info : [ 20%] Meshing curve 3 (Circle)
Info : [ 30%] Meshing curve 4 (Circle)
Info : [ 40%] Meshing curve 5 (Circle)
Info : [ 50%] Meshing curve 6 (Circle)
Info : [ 60%] Meshing curve 7 (Circle)
Info : [ 60%] Meshing curve 8 (Circle)
Info : [ 70%] Meshing curve 9 (Circle)
Info : [ 80%] Meshing curve 10 (Circle)
Info : [ 90%] Meshing curve 11 (Circle)
Info : [100%] Meshing curve 12 (Circle)
Info : Done meshing 1D (Wall 0.00470433s, CPU 0.00232s)
Info : Meshing 2D...
Info : [ 0%] Meshing surface 14 (Surface, MeshAdapt)
Info : [ 20%] Meshing surface 16 (Surface, MeshAdapt)
Info : [ 30%] Meshing surface 18 (Surface, MeshAdapt)
Info : [ 40%] Meshing surface 20 (Surface, MeshAdapt)
Info : [ 60%] Meshing surface 22 (Surface, MeshAdapt)
Info : [ 70%] Meshing surface 24 (Surface, MeshAdapt)
Info : [ 80%] Meshing surface 26 (Surface, MeshAdapt)
Info : [ 90%] Meshing surface 28 (Surface, MeshAdapt)
Info : Done meshing 2D (Wall 87.4357s, CPU 33.8863s)
Info : 7669 nodes 15747 elements
Info : Writing 'sphere.msh'...
Info : Done writing 'sphere.msh'
Info : Stopped on Tue Jun 30 05:15:31 2026 (From start: Wall 87.7579s, CPU 34.0148s)
gmtmask: num vertices 7668
gmtmask: done
Step 2: Define loads in meters of ice height equivalent
1 of 1 months done!
Step 3: Parameterization
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In runme (line 65)]
Step 4: Solve Esa solver
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/EsaGRACE-06-30-2026-05-16-02-34841/EsaGRACE.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
starting model processor
creating datasets for analysis EsaAnalysis
updating elements and materials for control parameters
updating elements and materials for uncertainty quantification
creating output definitions
done with model processor
Processing finite element model of analysis EsaAnalysis:
toolkits Options set for analysis: EsaAnalysis
configuring element and loads
Configuring elements...
Configuring loads...
Configuring materials...
Configuring inputs...
detecting active vertices
resolving node constraints
creating nodal degrees of freedom
Renumbering degrees of freedom
call computational core:
computing elastic adjustment
toolkits Options set for analysis: EsaAnalysis
computing elastic geodetic core
write lock file:
FemModel initialization elapsed time: 0.401278
Total Core solution elapsed time: 22.7696
Linear solver elapsed time: 0 (0%)
Total elapsed time: 0 hrs 0 min 23 sec
WARNING! There are options you set that were not used!
WARNING! could be spelling mistake, etc!
There are 7 unused database options. They are:
Option left: name:-ksp_type value: preonly source: code
Option left: name:-mat_mumps_icntl_14 value: 120 source: code
Option left: name:-mat_mumps_icntl_28 value: 2 source: code
Option left: name:-mat_mumps_icntl_29 value: 2 source: code
Option left: name:-mat_type value: mpiaij source: code
Option left: name:-pc_factor_mat_solver_type value: mumps source: code
Option left: name:-pc_type value: lu source: code
loading results from cluster
Step 5: Plot solutions
SUCCESS
+++ exit code: 0
+++ error: 0
+++ Running case: Example-EsaWahr
+++ working dir: /Users/jenkins/workspace/macOS-Intel-Examples/nightlylog
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Mesh creation
Step 2: Anisotropic mesh creation
Anisotropic mesh adaptation
WARNING: mesh present but no geometry found. Reconstructing...
new number of triangles = 4207
Step 3: Define loads
Step 4: Parameterization
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In runme (line 73)]
Step 5: Solve Esa solver
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/EsaWahr-06-30-2026-05-17-19-45557/EsaWahr.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
starting model processor
creating datasets for analysis EsaAnalysis
updating elements and materials for control parameters
updating elements and materials for uncertainty quantification
creating output definitions
done with model processor
Processing finite element model of analysis EsaAnalysis:
toolkits Options set for analysis: EsaAnalysis
configuring element and loads
Configuring elements...
Configuring loads...
Configuring materials...
Configuring inputs...
detecting active vertices
resolving node constraints
creating nodal degrees of freedom
Renumbering degrees of freedom
call computational core:
computing elastic adjustment
toolkits Options set for analysis: EsaAnalysis
computing elastic geodetic core
write lock file:
FemModel initialization elapsed time: 0.18698
Total Core solution elapsed time: 0.832978
Linear solver elapsed time: 0 (0%)
Total elapsed time: 0 hrs 0 min 1 sec
WARNING! There are options you set that were not used!
WARNING! could be spelling mistake, etc!
There are 7 unused database options. They are:
Option left: name:-ksp_type value: preonly source: code
Option left: name:-mat_mumps_icntl_14 value: 120 source: code
Option left: name:-mat_mumps_icntl_28 value: 2 source: code
Option left: name:-mat_mumps_icntl_29 value: 2 source: code
Option left: name:-mat_type value: mpiaij source: code
Option left: name:-pc_factor_mat_solver_type value: mumps source: code
Option left: name:-pc_type value: lu source: code
loading results from cluster
Step 6: Plot solutions
Step 7: Compare results against Wahr semi-analytic solutions
SUCCESS
+++ exit code: 0
+++ error: 0
+++ Running case: Example-EsaWahr
+++ working dir: /Users/jenkins/workspace/macOS-Intel-Examples/nightlylog
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Mesh creation
Step 2: Anisotropic mesh creation
Anisotropic mesh adaptation
WARNING: mesh present but no geometry found. Reconstructing...
new number of triangles = 4207
Step 3: Define loads
Step 4: Parameterization
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In runme (line 73)]
Step 5: Solve Esa solver
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/EsaWahr-06-30-2026-05-17-19-45557/EsaWahr.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
starting model processor
creating datasets for analysis EsaAnalysis
updating elements and materials for control parameters
updating elements and materials for uncertainty quantification
creating output definitions
done with model processor
Processing finite element model of analysis EsaAnalysis:
toolkits Options set for analysis: EsaAnalysis
configuring element and loads
Configuring elements...
Configuring loads...
Configuring materials...
Configuring inputs...
detecting active vertices
resolving node constraints
creating nodal degrees of freedom
Renumbering degrees of freedom
call computational core:
computing elastic adjustment
toolkits Options set for analysis: EsaAnalysis
computing elastic geodetic core
write lock file:
FemModel initialization elapsed time: 0.18698
Total Core solution elapsed time: 0.832978
Linear solver elapsed time: 0 (0%)
Total elapsed time: 0 hrs 0 min 1 sec
WARNING! There are options you set that were not used!
WARNING! could be spelling mistake, etc!
There are 7 unused database options. They are:
Option left: name:-ksp_type value: preonly source: code
Option left: name:-mat_mumps_icntl_14 value: 120 source: code
Option left: name:-mat_mumps_icntl_28 value: 2 source: code
Option left: name:-mat_mumps_icntl_29 value: 2 source: code
Option left: name:-mat_type value: mpiaij source: code
Option left: name:-pc_factor_mat_solver_type value: mumps source: code
Option left: name:-pc_type value: lu source: code
loading results from cluster
Step 6: Plot solutions
Step 7: Compare results against Wahr semi-analytic solutions
SUCCESS
+++ exit code: 0
+++ error: 0
+++ Running case: Example-Greenland
+++ working dir: /Users/jenkins/workspace/macOS-Intel-Examples/nightlylog
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Mesh creation
Anisotropic mesh adaptation
WARNING: mesh present but no geometry found. Reconstructing...
new number of triangles = 6345
Step 2: Parameterization
Loading SeaRISE data from NetCDF
Interpolating surface and bedrock
Constructing thickness
Interpolating velocities
Interpolating temperatures
Interpolating surface mass balance
Construct basal friction parameters
Construct ice rheological properties
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In TemporaryParameterFile57804 (line 54)
In parameterize (line 29)
In runme (line 41)]
Set other boundary conditions
Set geothermal heat flux
Set Pressure
Single point constraints
Step 3: Control method friction
checking model consistency
INFO: the outlog will look better if only md.verbose.control is turned on
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-17-52-57804/SeaRISEgreenland.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
call computational core:
preparing initial solution
x | Cost function f(x) | List of contributions
====================== step 1/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 59172.79 | 7092.887 52079.9 6.085212e-32
x = 1 | f(x) = 50954.87 | 3600.244 47354.58 0.04587451
====================== step 2/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 50953.45 | 3598.809 47354.6 0.04587451
x = 1 | f(x) = 44978.74 | 2137.679 42840.82 0.2370654
====================== step 3/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 44987.02 | 2146.197 42840.58 0.2370654
x = 1 | f(x) = 44425.8 | 2044.873 42380.66 0.2722667
====================== step 4/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 44432.36 | 2051.851 42380.24 0.2722667
x = 1 | f(x) = 42775.97 | 1747.394 41028.16 0.4148691
====================== step 5/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 42783.98 | 1756.726 41026.84 0.4148691
x = 1 | f(x) = 41876.1 | 1659.336 40216.23 0.5302616
====================== step 6/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 41885.98 | 1670.347 40215.1 0.5302616
x = 1 | f(x) = 40869.39 | 1561.173 39307.52 0.6932322
====================== step 7/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 40870.91 | 1563.273 39306.95 0.6932322
x = 1 | f(x) = 39697.76 | 1338.256 38358.58 0.9236775
====================== step 8/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 39697.43 | 1338.655 38357.85 0.9236775
x = 1 | f(x) = 39040.22 | 1208.675 37830.47 1.071791
====================== step 9/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 39039.49 | 1208.558 37829.86 1.071791
x = 1 | f(x) = 38556.09 | 1126.764 37428.13 1.191478
====================== step 10/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 38552.98 | 1124.507 37427.28 1.191478
x = 1 | f(x) = 38121.56 | 1092.495 37027.74 1.3288
====================== step 11/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 38122.77 | 1094.958 37026.49 1.3288
x = 1 | f(x) = 37729.41 | 1149.628 36578.29 1.493932
====================== step 12/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37740.46 | 1159.142 36579.82 1.493932
x = 1 | f(x) = 37487.92 | 1087.186 36399.14 1.592633
x = 0.381966 | f(x) = 37611.19 | 1112.303 36497.36 1.529775
x = 0.618034 | f(x) = 37561.1 | 1101.089 36458.46 1.55338
x = 0.763932 | f(x) = 37530.94 | 1093.798 36435.58 1.568476
x = 0.854102 | f(x) = 37512.65 | 1089.499 36421.58 1.577683
x = 0.90983 | f(x) = 37501.45 | 1086.979 36412.88 1.583344
====================== step 13/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37484.86 | 1084.592 36398.67 1.592633
x = 1 | f(x) = 37022.46 | 1018.285 36002.41 1.768007
====================== step 14/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37030.9 | 1026.085 36003.05 1.768007
x = 1 | f(x) = 36814.89 | 1058.135 35754.9 1.859438
x = 0.381966 | f(x) = 36898.13 | 989.5907 35906.74 1.799676
x = 0.618034 | f(x) = 36853.98 | 1003.884 35848.28 1.821225
x = 0.763932 | f(x) = 36838.62 | 1025.038 35811.75 1.835325
x = 0.937069 | f(x) = 36824.08 | 1052.478 35769.75 1.852853
x = 0.870937 | f(x) = 36839.21 | 1051.966 35785.4 1.846056
====================== step 15/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36824.8 | 1068.389 35754.55 1.859438
x = 1 | f(x) = 36559.07 | 954.0377 35603.09 1.936544
x = 0.381966 | f(x) = 36711.5 | 1017.403 35692.21 1.887487
x = 0.618034 | f(x) = 36653.71 | 995.7569 35656.05 1.905392
x = 0.763932 | f(x) = 36614.76 | 978.0481 35634.8 1.916939
x = 0.854102 | f(x) = 36589.85 | 965.9689 35621.95 1.92432
x = 0.90983 | f(x) = 36574.06 | 958.1749 35613.95 1.928974
====================== step 16/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36552.27 | 948.6767 35601.65 1.936544
x = 1 | f(x) = 36368.74 | 909.4905 35457.24 2.009954
x = 0.381966 | f(x) = 36450.66 | 912.2196 35536.48 1.964688
x = 0.618034 | f(x) = 36415.28 | 905.8741 35507.42 1.981913
x = 0.763932 | f(x) = 36394.68 | 904.2792 35488.41 1.992565
x = 0.854102 | f(x) = 36384.31 | 906.0028 35476.31 1.999281
x = 0.90983 | f(x) = 36379.73 | 908.9319 35468.79 2.003357
====================== step 17/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36373.34 | 914.7542 35456.58 2.009954
x = 1 | f(x) = 36229.12 | 957.6674 35269.34 2.111313
x = 0.381966 | f(x) = 36289.06 | 905.1848 35381.82 2.046875
x = 0.618034 | f(x) = 36257.86 | 916.5034 35339.28 2.070593
x = 0.763932 | f(x) = 36247.49 | 932.6872 35312.72 2.085785
x = 0.913021 | f(x) = 36239.38 | 951.6387 35285.64 2.101794
x = 0.856074 | f(x) = 36249.62 | 951.977 35295.55 2.095621
====================== step 18/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36238.23 | 966.1893 35269.93 2.111313
x = 1 | f(x) = 36005.81 | 893.306 35110.31 2.18899
x = 0.381966 | f(x) = 36142.54 | 929.6447 35210.76 2.139784
x = 0.618034 | f(x) = 36093.23 | 916.1558 35174.92 2.158128
x = 0.763932 | f(x) = 36058.58 | 905.5225 35150.89 2.16975
x = 0.854102 | f(x) = 36036.9 | 898.7214 35136 2.177043
x = 0.90983 | f(x) = 36023.73 | 894.6151 35126.93 2.18159
====================== step 19/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36005.22 | 890.2107 35112.82 2.18899
x = 1 | f(x) = 35868.42 | 869.9581 34996.18 2.287732
x = 0.381966 | f(x) = 35911.39 | 860.1821 35048.98 2.225541
x = 0.618034 | f(x) = 35893.04 | 858.0691 35032.72 2.249067
x = 0.763932 | f(x) = 35881.94 | 859.7353 35019.94 2.263658
x = 0.854102 | f(x) = 35877.04 | 863.763 35011.01 2.272799
x = 0.90983 | f(x) = 35875.47 | 868.0771 35005.11 2.278502
====================== step 20/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35873.35 | 875.6681 34995.4 2.287732
x = 1 | f(x) = 35723.35 | 910.5513 34810.43 2.374027
x = 0.381966 | f(x) = 35789.66 | 860.5594 34926.79 2.319061
x = 0.618034 | f(x) = 35757.04 | 868.789 34885.91 2.339232
x = 0.763932 | f(x) = 35744.03 | 883.7317 34857.95 2.352231
x = 0.854102 | f(x) = 35739.94 | 897.5494 34840.03 2.360435
x = 0.930997 | f(x) = 35737.52 | 910.28 34824.87 2.367548
====================== step 21/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35735.84 | 922.2347 34811.23 2.374027
x = 1 | f(x) = 35602.51 | 870.7784 34729.3 2.423398
x = 0.381966 | f(x) = 35668.82 | 880.0971 34786.33 2.391628
x = 0.618034 | f(x) = 35644.9 | 872.7159 34769.79 2.403223
x = 0.763932 | f(x) = 35629.08 | 870.0702 34756.6 2.410606
x = 0.854102 | f(x) = 35618.25 | 868.4465 34747.39 2.415368
x = 0.90983 | f(x) = 35610.89 | 867.4925 34740.98 2.418388
====================== step 22/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35599.85 | 867.5045 34729.92 2.423398
x = 1 | f(x) = 35435.33 | 841.7746 34591.04 2.515761
x = 0.381966 | f(x) = 35503.09 | 830.83 34669.8 2.457304
x = 0.618034 | f(x) = 35463.09 | 825.8312 34634.77 2.479098
x = 0.763932 | f(x) = 35440.81 | 828.0732 34610.24 2.492898
x = 0.854102 | f(x) = 35432.56 | 834.5397 34595.51 2.501553
x = 0.90983 | f(x) = 35438.35 | 841.9242 34593.91 2.50695
====================== step 23/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35439.26 | 840.4865 34596.27 2.501553
x = 1 | f(x) = 35377.76 | 827.9225 34547.29 2.55107
x = 0.381966 | f(x) = 35416.76 | 819.8319 34594.41 2.518729
x = 0.618034 | f(x) = 35399.79 | 819.4099 34577.85 2.530419
x = 0.763932 | f(x) = 35393.8 | 822.2266 34569.04 2.538053
x = 0.944313 | f(x) = 35386.99 | 828.3334 34556.1 2.547926
x = 0.875413 | f(x) = 35393.31 | 829.0398 34561.73 2.544098
====================== step 24/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35389.05 | 833.3283 34553.17 2.55107
x = 1 | f(x) = 35252.08 | 814.3328 34435.09 2.649675
x = 0.381966 | f(x) = 35317.08 | 812.978 34501.52 2.588143
x = 0.618034 | f(x) = 35288.37 | 809.7173 34476.04 2.611631
x = 0.763932 | f(x) = 35271.33 | 809.3561 34459.34 2.626304
x = 0.854102 | f(x) = 35263.63 | 811.1878 34449.81 2.635229
x = 0.90983 | f(x) = 35260.58 | 813.8445 34444.09 2.640723
====================== step 25/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35256.61 | 818.8748 34435.09 2.649675
x = 1 | f(x) = 35162.53 | 858.2923 34301.5 2.735676
x = 0.381966 | f(x) = 35180.62 | 812.9346 34365.01 2.680864
x = 0.618034 | f(x) = 35153.13 | 821.9691 34328.46 2.701321
x = 0.763932 | f(x) = 35158.4 | 837.054 34318.64 2.714146
x = 0.645763 | f(x) = 35167.63 | 833.394 34331.53 2.703727
x = 0.527864 | f(x) = 35170.22 | 824.2448 34343.28 2.693583
====================== step 26/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35160.91 | 827.091 34331.12 2.701321
x = 1 | f(x) = 35121.46 | 799.6831 34319.05 2.727669
x = 0.381966 | f(x) = 35148.31 | 811.7235 34333.88 2.710518
x = 0.618034 | f(x) = 35139.87 | 807.5893 34329.56 2.716727
x = 0.763932 | f(x) = 35133.07 | 803.7521 34326.59 2.720776
x = 0.854102 | f(x) = 35127.96 | 801.0169 34324.22 2.723359
x = 0.90983 | f(x) = 35124.32 | 799.2107 34322.38 2.724986
====================== step 27/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35118.96 | 797.3025 34318.93 2.727669
x = 1 | f(x) = 34992.01 | 809.2473 34179.93 2.832751
x = 0.381966 | f(x) = 35054.02 | 790.9422 34260.31 2.766228
x = 0.618034 | f(x) = 35029.18 | 793.4468 34232.94 2.790931
x = 0.763932 | f(x) = 35015.1 | 799.223 34213.07 2.806635
x = 0.854102 | f(x) = 35009.09 | 806.1057 34200.17 2.816507
x = 0.90983 | f(x) = 35007.38 | 812.598 34191.96 2.822672
====================== step 28/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35004.32 | 822.0413 34179.44 2.832751
x = 1 | f(x) = 34934.87 | 806.5674 34125.43 2.869513
x = 0.381966 | f(x) = 34947.17 | 786.7793 34157.54 2.846471
x = 0.618034 | f(x) = 34937.13 | 788.8927 34145.38 2.855048
x = 0.763932 | f(x) = 34935.7 | 795.0416 34137.8 2.860456
x = 0.748008 | f(x) = 34937.94 | 796.546 34138.54 2.859861
x = 0.854102 | f(x) = 34938.57 | 802.5726 34133.14 2.863862
====================== step 29/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 34941.3 | 812.7678 34125.66 2.869513
x = 1 | f(x) = 34824.78 | 779.576 34042.26 2.935698
x = 0.381966 | f(x) = 34880.03 | 788.1485 34088.99 2.894439
x = 0.618034 | f(x) = 34858.6 | 784.1171 34071.57 2.91002
x = 0.763932 | f(x) = 34843.88 | 780.8715 34060.09 2.919804
x = 0.854102 | f(x) = 34835.32 | 779.3894 34053.01 2.925896
x = 0.90983 | f(x) = 34830.74 | 779.0445 34048.76 2.929623
====================== step 30/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 34824.9 | 779.6846 34042.28 2.935698
x = 1 | f(x) = 34721.73 | 773.8226 33944.9 3.012811
x = 0.381966 | f(x) = 34777.78 | 771.9937 34002.82 2.964712
x = 0.618034 | f(x) = 34756.76 | 772.5218 33981.26 2.983082
x = 0.763932 | f(x) = 34743.45 | 772.8096 33967.65 2.994363
x = 0.854102 | f(x) = 34735.33 | 773.2066 33959.12 3.001402
x = 0.90983 | f(x) = 34730.47 | 773.6083 33953.86 3.005763
preparing final solution
computing new velocity
write lock file:
FemModel initialization elapsed time: 0.134429
Total Core solution elapsed time: 97.4304
Linear solver elapsed time: 58.3618 (60%)
Total elapsed time: 0 hrs 1 min 37 sec
loading results from cluster
Step 4: Transient run
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-19-39-57804/SeaRISEgreenland.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
Input updates from constant
Input updates from constant
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
call computational core:
Updating Mmes
iteration 1/100 time [yr]: 0.20 (time step: 0.20)
computing smb
computing new velocity
Updating constraints and active domain of analysis StressbalanceAnalysis for time: 0.2
Get solution from inputs
Reduce vector from g to f set
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.05155e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 41.3709 > 1 %
Convergence criterion: norm(du)/norm(u) 63.1692 > 10 %
Convergence criterion: max(du) 0.000157031
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.08287e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 3.67351 > 1 %
Convergence criterion: norm(du)/norm(u) 7.15747 < 10 %
Convergence criterion: max(du) 8.86618e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.21945e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 1.10917 > 1 %
Convergence criterion: norm(du)/norm(u) 2.86495 < 10 %
Convergence criterion: max(du) 5.14918e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.01372e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 0.445157 < 1 %
Convergence criterion: norm(du)/norm(u) 1.23492 < 10 %
Convergence criterion: max(du) 2.12087e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
total number of iterations: 4
computing basal mass balance
computing mass transport
Updating constraints and active domain of analysis MasstransportAnalysis for time: 0.2
Allocating matrices
[1] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[1] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
(Kff stiffness matrix size: 3699 x 3699)
Assembling matrices
[0] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[0] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
loading results from cluster
[Warning: Could not copy
/Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-19-39-57804//SeaRISEgreenland.outbin]
[> In issmscpin (line 22)
In generic/Download (line 328)
In loadresultsfromcluster (line 45)
In solve (line 210)
In runme (line 111)]
Error using loadresultsfromdisk
=========================================================================
Binary file SeaRISEgreenland.outbin not found
This typically results from an error encountered during the simulation
Please check for error messages above or in the outlog
=========================================================================
Error in loadresultsfromcluster (line 48)
md=loadresultsfromdisk(md,d.miscellaneous.name '.outbin']);
Error in solve (line 210)
md=loadresultsfromcluster(md);
Error in runme (line 111)
md=solve(md,'Transient');FAILURE
+++ exit code: 0
+++ error: 0
+++ Running case: Example-Greenland
+++ working dir: /Users/jenkins/workspace/macOS-Intel-Examples/nightlylog
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Mesh creation
Anisotropic mesh adaptation
WARNING: mesh present but no geometry found. Reconstructing...
new number of triangles = 6345
Step 2: Parameterization
Loading SeaRISE data from NetCDF
Interpolating surface and bedrock
Constructing thickness
Interpolating velocities
Interpolating temperatures
Interpolating surface mass balance
Construct basal friction parameters
Construct ice rheological properties
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In TemporaryParameterFile57804 (line 54)
In parameterize (line 29)
In runme (line 41)]
Set other boundary conditions
Set geothermal heat flux
Set Pressure
Single point constraints
Step 3: Control method friction
checking model consistency
INFO: the outlog will look better if only md.verbose.control is turned on
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-17-52-57804/SeaRISEgreenland.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
call computational core:
preparing initial solution
x | Cost function f(x) | List of contributions
====================== step 1/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 59172.79 | 7092.887 52079.9 6.085212e-32
x = 1 | f(x) = 50954.87 | 3600.244 47354.58 0.04587451
====================== step 2/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 50953.45 | 3598.809 47354.6 0.04587451
x = 1 | f(x) = 44978.74 | 2137.679 42840.82 0.2370654
====================== step 3/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 44987.02 | 2146.197 42840.58 0.2370654
x = 1 | f(x) = 44425.8 | 2044.873 42380.66 0.2722667
====================== step 4/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 44432.36 | 2051.851 42380.24 0.2722667
x = 1 | f(x) = 42775.97 | 1747.394 41028.16 0.4148691
====================== step 5/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 42783.98 | 1756.726 41026.84 0.4148691
x = 1 | f(x) = 41876.1 | 1659.336 40216.23 0.5302616
====================== step 6/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 41885.98 | 1670.347 40215.1 0.5302616
x = 1 | f(x) = 40869.39 | 1561.173 39307.52 0.6932322
====================== step 7/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 40870.91 | 1563.273 39306.95 0.6932322
x = 1 | f(x) = 39697.76 | 1338.256 38358.58 0.9236775
====================== step 8/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 39697.43 | 1338.655 38357.85 0.9236775
x = 1 | f(x) = 39040.22 | 1208.675 37830.47 1.071791
====================== step 9/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 39039.49 | 1208.558 37829.86 1.071791
x = 1 | f(x) = 38556.09 | 1126.764 37428.13 1.191478
====================== step 10/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 38552.98 | 1124.507 37427.28 1.191478
x = 1 | f(x) = 38121.56 | 1092.495 37027.74 1.3288
====================== step 11/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 38122.77 | 1094.958 37026.49 1.3288
x = 1 | f(x) = 37729.41 | 1149.628 36578.29 1.493932
====================== step 12/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37740.46 | 1159.142 36579.82 1.493932
x = 1 | f(x) = 37487.92 | 1087.186 36399.14 1.592633
x = 0.381966 | f(x) = 37611.19 | 1112.303 36497.36 1.529775
x = 0.618034 | f(x) = 37561.1 | 1101.089 36458.46 1.55338
x = 0.763932 | f(x) = 37530.94 | 1093.798 36435.58 1.568476
x = 0.854102 | f(x) = 37512.65 | 1089.499 36421.58 1.577683
x = 0.90983 | f(x) = 37501.45 | 1086.979 36412.88 1.583344
====================== step 13/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37484.86 | 1084.592 36398.67 1.592633
x = 1 | f(x) = 37022.46 | 1018.285 36002.41 1.768007
====================== step 14/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37030.9 | 1026.085 36003.05 1.768007
x = 1 | f(x) = 36814.89 | 1058.135 35754.9 1.859438
x = 0.381966 | f(x) = 36898.13 | 989.5907 35906.74 1.799676
x = 0.618034 | f(x) = 36853.98 | 1003.884 35848.28 1.821225
x = 0.763932 | f(x) = 36838.62 | 1025.038 35811.75 1.835325
x = 0.937069 | f(x) = 36824.08 | 1052.478 35769.75 1.852853
x = 0.870937 | f(x) = 36839.21 | 1051.966 35785.4 1.846056
====================== step 15/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36824.8 | 1068.389 35754.55 1.859438
x = 1 | f(x) = 36559.07 | 954.0377 35603.09 1.936544
x = 0.381966 | f(x) = 36711.5 | 1017.403 35692.21 1.887487
x = 0.618034 | f(x) = 36653.71 | 995.7569 35656.05 1.905392
x = 0.763932 | f(x) = 36614.76 | 978.0481 35634.8 1.916939
x = 0.854102 | f(x) = 36589.85 | 965.9689 35621.95 1.92432
x = 0.90983 | f(x) = 36574.06 | 958.1749 35613.95 1.928974
====================== step 16/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36552.27 | 948.6767 35601.65 1.936544
x = 1 | f(x) = 36368.74 | 909.4905 35457.24 2.009954
x = 0.381966 | f(x) = 36450.66 | 912.2196 35536.48 1.964688
x = 0.618034 | f(x) = 36415.28 | 905.8741 35507.42 1.981913
x = 0.763932 | f(x) = 36394.68 | 904.2792 35488.41 1.992565
x = 0.854102 | f(x) = 36384.31 | 906.0028 35476.31 1.999281
x = 0.90983 | f(x) = 36379.73 | 908.9319 35468.79 2.003357
====================== step 17/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36373.34 | 914.7542 35456.58 2.009954
x = 1 | f(x) = 36229.12 | 957.6674 35269.34 2.111313
x = 0.381966 | f(x) = 36289.06 | 905.1848 35381.82 2.046875
x = 0.618034 | f(x) = 36257.86 | 916.5034 35339.28 2.070593
x = 0.763932 | f(x) = 36247.49 | 932.6872 35312.72 2.085785
x = 0.913021 | f(x) = 36239.38 | 951.6387 35285.64 2.101794
x = 0.856074 | f(x) = 36249.62 | 951.977 35295.55 2.095621
====================== step 18/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36238.23 | 966.1893 35269.93 2.111313
x = 1 | f(x) = 36005.81 | 893.306 35110.31 2.18899
x = 0.381966 | f(x) = 36142.54 | 929.6447 35210.76 2.139784
x = 0.618034 | f(x) = 36093.23 | 916.1558 35174.92 2.158128
x = 0.763932 | f(x) = 36058.58 | 905.5225 35150.89 2.16975
x = 0.854102 | f(x) = 36036.9 | 898.7214 35136 2.177043
x = 0.90983 | f(x) = 36023.73 | 894.6151 35126.93 2.18159
====================== step 19/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36005.22 | 890.2107 35112.82 2.18899
x = 1 | f(x) = 35868.42 | 869.9581 34996.18 2.287732
x = 0.381966 | f(x) = 35911.39 | 860.1821 35048.98 2.225541
x = 0.618034 | f(x) = 35893.04 | 858.0691 35032.72 2.249067
x = 0.763932 | f(x) = 35881.94 | 859.7353 35019.94 2.263658
x = 0.854102 | f(x) = 35877.04 | 863.763 35011.01 2.272799
x = 0.90983 | f(x) = 35875.47 | 868.0771 35005.11 2.278502
====================== step 20/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35873.35 | 875.6681 34995.4 2.287732
x = 1 | f(x) = 35723.35 | 910.5513 34810.43 2.374027
x = 0.381966 | f(x) = 35789.66 | 860.5594 34926.79 2.319061
x = 0.618034 | f(x) = 35757.04 | 868.789 34885.91 2.339232
x = 0.763932 | f(x) = 35744.03 | 883.7317 34857.95 2.352231
x = 0.854102 | f(x) = 35739.94 | 897.5494 34840.03 2.360435
x = 0.930997 | f(x) = 35737.52 | 910.28 34824.87 2.367548
====================== step 21/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35735.84 | 922.2347 34811.23 2.374027
x = 1 | f(x) = 35602.51 | 870.7784 34729.3 2.423398
x = 0.381966 | f(x) = 35668.82 | 880.0971 34786.33 2.391628
x = 0.618034 | f(x) = 35644.9 | 872.7159 34769.79 2.403223
x = 0.763932 | f(x) = 35629.08 | 870.0702 34756.6 2.410606
x = 0.854102 | f(x) = 35618.25 | 868.4465 34747.39 2.415368
x = 0.90983 | f(x) = 35610.89 | 867.4925 34740.98 2.418388
====================== step 22/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35599.85 | 867.5045 34729.92 2.423398
x = 1 | f(x) = 35435.33 | 841.7746 34591.04 2.515761
x = 0.381966 | f(x) = 35503.09 | 830.83 34669.8 2.457304
x = 0.618034 | f(x) = 35463.09 | 825.8312 34634.77 2.479098
x = 0.763932 | f(x) = 35440.81 | 828.0732 34610.24 2.492898
x = 0.854102 | f(x) = 35432.56 | 834.5397 34595.51 2.501553
x = 0.90983 | f(x) = 35438.35 | 841.9242 34593.91 2.50695
====================== step 23/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35439.26 | 840.4865 34596.27 2.501553
x = 1 | f(x) = 35377.76 | 827.9225 34547.29 2.55107
x = 0.381966 | f(x) = 35416.76 | 819.8319 34594.41 2.518729
x = 0.618034 | f(x) = 35399.79 | 819.4099 34577.85 2.530419
x = 0.763932 | f(x) = 35393.8 | 822.2266 34569.04 2.538053
x = 0.944313 | f(x) = 35386.99 | 828.3334 34556.1 2.547926
x = 0.875413 | f(x) = 35393.31 | 829.0398 34561.73 2.544098
====================== step 24/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35389.05 | 833.3283 34553.17 2.55107
x = 1 | f(x) = 35252.08 | 814.3328 34435.09 2.649675
x = 0.381966 | f(x) = 35317.08 | 812.978 34501.52 2.588143
x = 0.618034 | f(x) = 35288.37 | 809.7173 34476.04 2.611631
x = 0.763932 | f(x) = 35271.33 | 809.3561 34459.34 2.626304
x = 0.854102 | f(x) = 35263.63 | 811.1878 34449.81 2.635229
x = 0.90983 | f(x) = 35260.58 | 813.8445 34444.09 2.640723
====================== step 25/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35256.61 | 818.8748 34435.09 2.649675
x = 1 | f(x) = 35162.53 | 858.2923 34301.5 2.735676
x = 0.381966 | f(x) = 35180.62 | 812.9346 34365.01 2.680864
x = 0.618034 | f(x) = 35153.13 | 821.9691 34328.46 2.701321
x = 0.763932 | f(x) = 35158.4 | 837.054 34318.64 2.714146
x = 0.645763 | f(x) = 35167.63 | 833.394 34331.53 2.703727
x = 0.527864 | f(x) = 35170.22 | 824.2448 34343.28 2.693583
====================== step 26/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35160.91 | 827.091 34331.12 2.701321
x = 1 | f(x) = 35121.46 | 799.6831 34319.05 2.727669
x = 0.381966 | f(x) = 35148.31 | 811.7235 34333.88 2.710518
x = 0.618034 | f(x) = 35139.87 | 807.5893 34329.56 2.716727
x = 0.763932 | f(x) = 35133.07 | 803.7521 34326.59 2.720776
x = 0.854102 | f(x) = 35127.96 | 801.0169 34324.22 2.723359
x = 0.90983 | f(x) = 35124.32 | 799.2107 34322.38 2.724986
====================== step 27/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35118.96 | 797.3025 34318.93 2.727669
x = 1 | f(x) = 34992.01 | 809.2473 34179.93 2.832751
x = 0.381966 | f(x) = 35054.02 | 790.9422 34260.31 2.766228
x = 0.618034 | f(x) = 35029.18 | 793.4468 34232.94 2.790931
x = 0.763932 | f(x) = 35015.1 | 799.223 34213.07 2.806635
x = 0.854102 | f(x) = 35009.09 | 806.1057 34200.17 2.816507
x = 0.90983 | f(x) = 35007.38 | 812.598 34191.96 2.822672
====================== step 28/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35004.32 | 822.0413 34179.44 2.832751
x = 1 | f(x) = 34934.87 | 806.5674 34125.43 2.869513
x = 0.381966 | f(x) = 34947.17 | 786.7793 34157.54 2.846471
x = 0.618034 | f(x) = 34937.13 | 788.8927 34145.38 2.855048
x = 0.763932 | f(x) = 34935.7 | 795.0416 34137.8 2.860456
x = 0.748008 | f(x) = 34937.94 | 796.546 34138.54 2.859861
x = 0.854102 | f(x) = 34938.57 | 802.5726 34133.14 2.863862
====================== step 29/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 34941.3 | 812.7678 34125.66 2.869513
x = 1 | f(x) = 34824.78 | 779.576 34042.26 2.935698
x = 0.381966 | f(x) = 34880.03 | 788.1485 34088.99 2.894439
x = 0.618034 | f(x) = 34858.6 | 784.1171 34071.57 2.91002
x = 0.763932 | f(x) = 34843.88 | 780.8715 34060.09 2.919804
x = 0.854102 | f(x) = 34835.32 | 779.3894 34053.01 2.925896
x = 0.90983 | f(x) = 34830.74 | 779.0445 34048.76 2.929623
====================== step 30/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 34824.9 | 779.6846 34042.28 2.935698
x = 1 | f(x) = 34721.73 | 773.8226 33944.9 3.012811
x = 0.381966 | f(x) = 34777.78 | 771.9937 34002.82 2.964712
x = 0.618034 | f(x) = 34756.76 | 772.5218 33981.26 2.983082
x = 0.763932 | f(x) = 34743.45 | 772.8096 33967.65 2.994363
x = 0.854102 | f(x) = 34735.33 | 773.2066 33959.12 3.001402
x = 0.90983 | f(x) = 34730.47 | 773.6083 33953.86 3.005763
preparing final solution
computing new velocity
write lock file:
FemModel initialization elapsed time: 0.134429
Total Core solution elapsed time: 97.4304
Linear solver elapsed time: 58.3618 (60%)
Total elapsed time: 0 hrs 1 min 37 sec
loading results from cluster
Step 4: Transient run
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-19-39-57804/SeaRISEgreenland.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
Input updates from constant
Input updates from constant
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
call computational core:
Updating Mmes
iteration 1/100 time [yr]: 0.20 (time step: 0.20)
computing smb
computing new velocity
Updating constraints and active domain of analysis StressbalanceAnalysis for time: 0.2
Get solution from inputs
Reduce vector from g to f set
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.05155e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 41.3709 > 1 %
Convergence criterion: norm(du)/norm(u) 63.1692 > 10 %
Convergence criterion: max(du) 0.000157031
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.08287e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 3.67351 > 1 %
Convergence criterion: norm(du)/norm(u) 7.15747 < 10 %
Convergence criterion: max(du) 8.86618e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.21945e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 1.10917 > 1 %
Convergence criterion: norm(du)/norm(u) 2.86495 < 10 %
Convergence criterion: max(du) 5.14918e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.01372e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 0.445157 < 1 %
Convergence criterion: norm(du)/norm(u) 1.23492 < 10 %
Convergence criterion: max(du) 2.12087e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
total number of iterations: 4
computing basal mass balance
computing mass transport
Updating constraints and active domain of analysis MasstransportAnalysis for time: 0.2
Allocating matrices
[1] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[1] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
(Kff stiffness matrix size: 3699 x 3699)
Assembling matrices
[0] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[0] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
loading results from cluster
[Warning: Could not copy
/Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-19-39-57804//SeaRISEgreenland.outbin]
[> In issmscpin (line 22)
In generic/Download (line 328)
In loadresultsfromcluster (line 45)
In solve (line 210)
In runme (line 111)]
Error using loadresultsfromdisk
=========================================================================
Binary file SeaRISEgreenland.outbin not found
This typically results from an error encountered during the simulation
Please check for error messages above or in the outlog
=========================================================================
Error in loadresultsfromcluster (line 48)
md=loadresultsfromdisk(md,d.miscellaneous.name '.outbin']);
Error in solve (line 210)
md=loadresultsfromcluster(md);
Error in runme (line 111)
md=solve(md,'Transient');FAILURE
+++ exit code: 0
+++ error: 1
----------MATLAB exited in error!----------
starting: AMR
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Coarse mesh
Construction of a mesh from a given geometry
Step 2: Parameterization
boundary conditions for stressbalance model: spc set as zero
no smb.mass_balance specified: values set as zero
no basalforcings.groundedice_melting_rate specified: values set as zero
no basalforcings.floatingice_melting_rate specified: values set as zero
no balancethickness.thickening_rate specified: values set as zero
no thermal boundary conditions created: no observed temperature found
Step 3: Solve!
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/mismip-06-30-2026-05-13-28-32501/mismip.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
call computational core:
iteration 1/500 time [yr]: 1.00 (time step: 1.00)
computing smb
computing new velocity
computing basal mass balance
computing mass transport
[0] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[0] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
[1] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[1] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
loading results from cluster
[Warning: Could not copy
/Users/jenkins/workspace/macOS-Intel-Examples//execution/mismip-06-30-2026-05-13-28-32501//mismip.outbin]
[> In issmscpin (line 22)
In generic/Download (line 328)
In loadresultsfromcluster (line 45)
In solve (line 210)
In runme (line 65)]
Error using loadresultsfromdisk
=========================================================================
Binary file mismip.outbin not found
This typically results from an error encountered during the simulation
Please check for error messages above or in the outlog
=========================================================================
Error in loadresultsfromcluster (line 48)
md=loadresultsfromdisk(md,d.miscellaneous.name '.outbin']);
Error in solve (line 210)
md=loadresultsfromcluster(md);
Error in runme (line 65)
md=solve(md,'Transient');FAILURE
finished: AMR
starting: EsaGRACE
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Global mesh creation
Info : Running 'gmsh -2 sphere.geo' [Gmsh 4.14.2-git-0cebcd9, 1 node, max. 1 thread]
Info : Started on Tue Jun 30 05:14:04 2026
Info : Reading 'sphere.geo'...
Info : Done reading 'sphere.geo'
Info : Meshing 1D...
Info : [ 0%] Meshing curve 1 (Circle)
Info : [ 10%] Meshing curve 2 (Circle)
Info : [ 20%] Meshing curve 3 (Circle)
Info : [ 30%] Meshing curve 4 (Circle)
Info : [ 40%] Meshing curve 5 (Circle)
Info : [ 50%] Meshing curve 6 (Circle)
Info : [ 60%] Meshing curve 7 (Circle)
Info : [ 60%] Meshing curve 8 (Circle)
Info : [ 70%] Meshing curve 9 (Circle)
Info : [ 80%] Meshing curve 10 (Circle)
Info : [ 90%] Meshing curve 11 (Circle)
Info : [100%] Meshing curve 12 (Circle)
Info : Done meshing 1D (Wall 0.00470433s, CPU 0.00232s)
Info : Meshing 2D...
Info : [ 0%] Meshing surface 14 (Surface, MeshAdapt)
Info : [ 20%] Meshing surface 16 (Surface, MeshAdapt)
Info : [ 30%] Meshing surface 18 (Surface, MeshAdapt)
Info : [ 40%] Meshing surface 20 (Surface, MeshAdapt)
Info : [ 60%] Meshing surface 22 (Surface, MeshAdapt)
Info : [ 70%] Meshing surface 24 (Surface, MeshAdapt)
Info : [ 80%] Meshing surface 26 (Surface, MeshAdapt)
Info : [ 90%] Meshing surface 28 (Surface, MeshAdapt)
Info : Done meshing 2D (Wall 87.4357s, CPU 33.8863s)
Info : 7669 nodes 15747 elements
Info : Writing 'sphere.msh'...
Info : Done writing 'sphere.msh'
Info : Stopped on Tue Jun 30 05:15:31 2026 (From start: Wall 87.7579s, CPU 34.0148s)
gmtmask: num vertices 7668
gmtmask: done
Step 2: Define loads in meters of ice height equivalent
1 of 1 months done!
Step 3: Parameterization
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In runme (line 65)]
Step 4: Solve Esa solver
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/EsaGRACE-06-30-2026-05-16-02-34841/EsaGRACE.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
starting model processor
creating datasets for analysis EsaAnalysis
updating elements and materials for control parameters
updating elements and materials for uncertainty quantification
creating output definitions
done with model processor
Processing finite element model of analysis EsaAnalysis:
toolkits Options set for analysis: EsaAnalysis
configuring element and loads
Configuring elements...
Configuring loads...
Configuring materials...
Configuring inputs...
detecting active vertices
resolving node constraints
creating nodal degrees of freedom
Renumbering degrees of freedom
call computational core:
computing elastic adjustment
toolkits Options set for analysis: EsaAnalysis
computing elastic geodetic core
write lock file:
FemModel initialization elapsed time: 0.401278
Total Core solution elapsed time: 22.7696
Linear solver elapsed time: 0 (0%)
Total elapsed time: 0 hrs 0 min 23 sec
WARNING! There are options you set that were not used!
WARNING! could be spelling mistake, etc!
There are 7 unused database options. They are:
Option left: name:-ksp_type value: preonly source: code
Option left: name:-mat_mumps_icntl_14 value: 120 source: code
Option left: name:-mat_mumps_icntl_28 value: 2 source: code
Option left: name:-mat_mumps_icntl_29 value: 2 source: code
Option left: name:-mat_type value: mpiaij source: code
Option left: name:-pc_factor_mat_solver_type value: mumps source: code
Option left: name:-pc_type value: lu source: code
loading results from cluster
Step 5: Plot solutions
SUCCESS
finished: EsaGRACE
starting: EsaWahr
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Mesh creation
Step 2: Anisotropic mesh creation
Anisotropic mesh adaptation
WARNING: mesh present but no geometry found. Reconstructing...
new number of triangles = 4207
Step 3: Define loads
Step 4: Parameterization
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In runme (line 73)]
Step 5: Solve Esa solver
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/EsaWahr-06-30-2026-05-17-19-45557/EsaWahr.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
starting model processor
creating datasets for analysis EsaAnalysis
updating elements and materials for control parameters
updating elements and materials for uncertainty quantification
creating output definitions
done with model processor
Processing finite element model of analysis EsaAnalysis:
toolkits Options set for analysis: EsaAnalysis
configuring element and loads
Configuring elements...
Configuring loads...
Configuring materials...
Configuring inputs...
detecting active vertices
resolving node constraints
creating nodal degrees of freedom
Renumbering degrees of freedom
call computational core:
computing elastic adjustment
toolkits Options set for analysis: EsaAnalysis
computing elastic geodetic core
write lock file:
FemModel initialization elapsed time: 0.18698
Total Core solution elapsed time: 0.832978
Linear solver elapsed time: 0 (0%)
Total elapsed time: 0 hrs 0 min 1 sec
WARNING! There are options you set that were not used!
WARNING! could be spelling mistake, etc!
There are 7 unused database options. They are:
Option left: name:-ksp_type value: preonly source: code
Option left: name:-mat_mumps_icntl_14 value: 120 source: code
Option left: name:-mat_mumps_icntl_28 value: 2 source: code
Option left: name:-mat_mumps_icntl_29 value: 2 source: code
Option left: name:-mat_type value: mpiaij source: code
Option left: name:-pc_factor_mat_solver_type value: mumps source: code
Option left: name:-pc_type value: lu source: code
loading results from cluster
Step 6: Plot solutions
Step 7: Compare results against Wahr semi-analytic solutions
SUCCESS
finished: EsaWahr
starting: Greenland
< M A T L A B (R) >
Copyright 1984-2023 The MathWorks, Inc.
R2023b Update 6 (23.2.0.2485118) 64-bit (maci64)
December 28, 2023
To get started, type doc.
For product information, visit www.mathworks.com.
ISSM development path correctly loaded
Step 1: Mesh creation
Anisotropic mesh adaptation
WARNING: mesh present but no geometry found. Reconstructing...
new number of triangles = 6345
Step 2: Parameterization
Loading SeaRISE data from NetCDF
Interpolating surface and bedrock
Constructing thickness
Interpolating velocities
Interpolating temperatures
Interpolating surface mass balance
Construct basal friction parameters
Construct ice rheological properties
[Warning: paterson is outdated, please consider using cuffey instead]
[> In paterson (line 10)
In TemporaryParameterFile57804 (line 54)
In parameterize (line 29)
In runme (line 41)]
Set other boundary conditions
Set geothermal heat flux
Set Pressure
Single point constraints
Step 3: Control method friction
checking model consistency
INFO: the outlog will look better if only md.verbose.control is turned on
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-17-52-57804/SeaRISEgreenland.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
call computational core:
preparing initial solution
x | Cost function f(x) | List of contributions
====================== step 1/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 59172.79 | 7092.887 52079.9 6.085212e-32
x = 1 | f(x) = 50954.87 | 3600.244 47354.58 0.04587451
====================== step 2/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 50953.45 | 3598.809 47354.6 0.04587451
x = 1 | f(x) = 44978.74 | 2137.679 42840.82 0.2370654
====================== step 3/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 44987.02 | 2146.197 42840.58 0.2370654
x = 1 | f(x) = 44425.8 | 2044.873 42380.66 0.2722667
====================== step 4/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 44432.36 | 2051.851 42380.24 0.2722667
x = 1 | f(x) = 42775.97 | 1747.394 41028.16 0.4148691
====================== step 5/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 42783.98 | 1756.726 41026.84 0.4148691
x = 1 | f(x) = 41876.1 | 1659.336 40216.23 0.5302616
====================== step 6/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 41885.98 | 1670.347 40215.1 0.5302616
x = 1 | f(x) = 40869.39 | 1561.173 39307.52 0.6932322
====================== step 7/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 40870.91 | 1563.273 39306.95 0.6932322
x = 1 | f(x) = 39697.76 | 1338.256 38358.58 0.9236775
====================== step 8/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 39697.43 | 1338.655 38357.85 0.9236775
x = 1 | f(x) = 39040.22 | 1208.675 37830.47 1.071791
====================== step 9/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 39039.49 | 1208.558 37829.86 1.071791
x = 1 | f(x) = 38556.09 | 1126.764 37428.13 1.191478
====================== step 10/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 38552.98 | 1124.507 37427.28 1.191478
x = 1 | f(x) = 38121.56 | 1092.495 37027.74 1.3288
====================== step 11/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 38122.77 | 1094.958 37026.49 1.3288
x = 1 | f(x) = 37729.41 | 1149.628 36578.29 1.493932
====================== step 12/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37740.46 | 1159.142 36579.82 1.493932
x = 1 | f(x) = 37487.92 | 1087.186 36399.14 1.592633
x = 0.381966 | f(x) = 37611.19 | 1112.303 36497.36 1.529775
x = 0.618034 | f(x) = 37561.1 | 1101.089 36458.46 1.55338
x = 0.763932 | f(x) = 37530.94 | 1093.798 36435.58 1.568476
x = 0.854102 | f(x) = 37512.65 | 1089.499 36421.58 1.577683
x = 0.90983 | f(x) = 37501.45 | 1086.979 36412.88 1.583344
====================== step 13/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37484.86 | 1084.592 36398.67 1.592633
x = 1 | f(x) = 37022.46 | 1018.285 36002.41 1.768007
====================== step 14/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 37030.9 | 1026.085 36003.05 1.768007
x = 1 | f(x) = 36814.89 | 1058.135 35754.9 1.859438
x = 0.381966 | f(x) = 36898.13 | 989.5907 35906.74 1.799676
x = 0.618034 | f(x) = 36853.98 | 1003.884 35848.28 1.821225
x = 0.763932 | f(x) = 36838.62 | 1025.038 35811.75 1.835325
x = 0.937069 | f(x) = 36824.08 | 1052.478 35769.75 1.852853
x = 0.870937 | f(x) = 36839.21 | 1051.966 35785.4 1.846056
====================== step 15/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36824.8 | 1068.389 35754.55 1.859438
x = 1 | f(x) = 36559.07 | 954.0377 35603.09 1.936544
x = 0.381966 | f(x) = 36711.5 | 1017.403 35692.21 1.887487
x = 0.618034 | f(x) = 36653.71 | 995.7569 35656.05 1.905392
x = 0.763932 | f(x) = 36614.76 | 978.0481 35634.8 1.916939
x = 0.854102 | f(x) = 36589.85 | 965.9689 35621.95 1.92432
x = 0.90983 | f(x) = 36574.06 | 958.1749 35613.95 1.928974
====================== step 16/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36552.27 | 948.6767 35601.65 1.936544
x = 1 | f(x) = 36368.74 | 909.4905 35457.24 2.009954
x = 0.381966 | f(x) = 36450.66 | 912.2196 35536.48 1.964688
x = 0.618034 | f(x) = 36415.28 | 905.8741 35507.42 1.981913
x = 0.763932 | f(x) = 36394.68 | 904.2792 35488.41 1.992565
x = 0.854102 | f(x) = 36384.31 | 906.0028 35476.31 1.999281
x = 0.90983 | f(x) = 36379.73 | 908.9319 35468.79 2.003357
====================== step 17/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36373.34 | 914.7542 35456.58 2.009954
x = 1 | f(x) = 36229.12 | 957.6674 35269.34 2.111313
x = 0.381966 | f(x) = 36289.06 | 905.1848 35381.82 2.046875
x = 0.618034 | f(x) = 36257.86 | 916.5034 35339.28 2.070593
x = 0.763932 | f(x) = 36247.49 | 932.6872 35312.72 2.085785
x = 0.913021 | f(x) = 36239.38 | 951.6387 35285.64 2.101794
x = 0.856074 | f(x) = 36249.62 | 951.977 35295.55 2.095621
====================== step 18/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36238.23 | 966.1893 35269.93 2.111313
x = 1 | f(x) = 36005.81 | 893.306 35110.31 2.18899
x = 0.381966 | f(x) = 36142.54 | 929.6447 35210.76 2.139784
x = 0.618034 | f(x) = 36093.23 | 916.1558 35174.92 2.158128
x = 0.763932 | f(x) = 36058.58 | 905.5225 35150.89 2.16975
x = 0.854102 | f(x) = 36036.9 | 898.7214 35136 2.177043
x = 0.90983 | f(x) = 36023.73 | 894.6151 35126.93 2.18159
====================== step 19/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 36005.22 | 890.2107 35112.82 2.18899
x = 1 | f(x) = 35868.42 | 869.9581 34996.18 2.287732
x = 0.381966 | f(x) = 35911.39 | 860.1821 35048.98 2.225541
x = 0.618034 | f(x) = 35893.04 | 858.0691 35032.72 2.249067
x = 0.763932 | f(x) = 35881.94 | 859.7353 35019.94 2.263658
x = 0.854102 | f(x) = 35877.04 | 863.763 35011.01 2.272799
x = 0.90983 | f(x) = 35875.47 | 868.0771 35005.11 2.278502
====================== step 20/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35873.35 | 875.6681 34995.4 2.287732
x = 1 | f(x) = 35723.35 | 910.5513 34810.43 2.374027
x = 0.381966 | f(x) = 35789.66 | 860.5594 34926.79 2.319061
x = 0.618034 | f(x) = 35757.04 | 868.789 34885.91 2.339232
x = 0.763932 | f(x) = 35744.03 | 883.7317 34857.95 2.352231
x = 0.854102 | f(x) = 35739.94 | 897.5494 34840.03 2.360435
x = 0.930997 | f(x) = 35737.52 | 910.28 34824.87 2.367548
====================== step 21/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35735.84 | 922.2347 34811.23 2.374027
x = 1 | f(x) = 35602.51 | 870.7784 34729.3 2.423398
x = 0.381966 | f(x) = 35668.82 | 880.0971 34786.33 2.391628
x = 0.618034 | f(x) = 35644.9 | 872.7159 34769.79 2.403223
x = 0.763932 | f(x) = 35629.08 | 870.0702 34756.6 2.410606
x = 0.854102 | f(x) = 35618.25 | 868.4465 34747.39 2.415368
x = 0.90983 | f(x) = 35610.89 | 867.4925 34740.98 2.418388
====================== step 22/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35599.85 | 867.5045 34729.92 2.423398
x = 1 | f(x) = 35435.33 | 841.7746 34591.04 2.515761
x = 0.381966 | f(x) = 35503.09 | 830.83 34669.8 2.457304
x = 0.618034 | f(x) = 35463.09 | 825.8312 34634.77 2.479098
x = 0.763932 | f(x) = 35440.81 | 828.0732 34610.24 2.492898
x = 0.854102 | f(x) = 35432.56 | 834.5397 34595.51 2.501553
x = 0.90983 | f(x) = 35438.35 | 841.9242 34593.91 2.50695
====================== step 23/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35439.26 | 840.4865 34596.27 2.501553
x = 1 | f(x) = 35377.76 | 827.9225 34547.29 2.55107
x = 0.381966 | f(x) = 35416.76 | 819.8319 34594.41 2.518729
x = 0.618034 | f(x) = 35399.79 | 819.4099 34577.85 2.530419
x = 0.763932 | f(x) = 35393.8 | 822.2266 34569.04 2.538053
x = 0.944313 | f(x) = 35386.99 | 828.3334 34556.1 2.547926
x = 0.875413 | f(x) = 35393.31 | 829.0398 34561.73 2.544098
====================== step 24/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35389.05 | 833.3283 34553.17 2.55107
x = 1 | f(x) = 35252.08 | 814.3328 34435.09 2.649675
x = 0.381966 | f(x) = 35317.08 | 812.978 34501.52 2.588143
x = 0.618034 | f(x) = 35288.37 | 809.7173 34476.04 2.611631
x = 0.763932 | f(x) = 35271.33 | 809.3561 34459.34 2.626304
x = 0.854102 | f(x) = 35263.63 | 811.1878 34449.81 2.635229
x = 0.90983 | f(x) = 35260.58 | 813.8445 34444.09 2.640723
====================== step 25/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35256.61 | 818.8748 34435.09 2.649675
x = 1 | f(x) = 35162.53 | 858.2923 34301.5 2.735676
x = 0.381966 | f(x) = 35180.62 | 812.9346 34365.01 2.680864
x = 0.618034 | f(x) = 35153.13 | 821.9691 34328.46 2.701321
x = 0.763932 | f(x) = 35158.4 | 837.054 34318.64 2.714146
x = 0.645763 | f(x) = 35167.63 | 833.394 34331.53 2.703727
x = 0.527864 | f(x) = 35170.22 | 824.2448 34343.28 2.693583
====================== step 26/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35160.91 | 827.091 34331.12 2.701321
x = 1 | f(x) = 35121.46 | 799.6831 34319.05 2.727669
x = 0.381966 | f(x) = 35148.31 | 811.7235 34333.88 2.710518
x = 0.618034 | f(x) = 35139.87 | 807.5893 34329.56 2.716727
x = 0.763932 | f(x) = 35133.07 | 803.7521 34326.59 2.720776
x = 0.854102 | f(x) = 35127.96 | 801.0169 34324.22 2.723359
x = 0.90983 | f(x) = 35124.32 | 799.2107 34322.38 2.724986
====================== step 27/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35118.96 | 797.3025 34318.93 2.727669
x = 1 | f(x) = 34992.01 | 809.2473 34179.93 2.832751
x = 0.381966 | f(x) = 35054.02 | 790.9422 34260.31 2.766228
x = 0.618034 | f(x) = 35029.18 | 793.4468 34232.94 2.790931
x = 0.763932 | f(x) = 35015.1 | 799.223 34213.07 2.806635
x = 0.854102 | f(x) = 35009.09 | 806.1057 34200.17 2.816507
x = 0.90983 | f(x) = 35007.38 | 812.598 34191.96 2.822672
====================== step 28/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 35004.32 | 822.0413 34179.44 2.832751
x = 1 | f(x) = 34934.87 | 806.5674 34125.43 2.869513
x = 0.381966 | f(x) = 34947.17 | 786.7793 34157.54 2.846471
x = 0.618034 | f(x) = 34937.13 | 788.8927 34145.38 2.855048
x = 0.763932 | f(x) = 34935.7 | 795.0416 34137.8 2.860456
x = 0.748008 | f(x) = 34937.94 | 796.546 34138.54 2.859861
x = 0.854102 | f(x) = 34938.57 | 802.5726 34133.14 2.863862
====================== step 29/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 34941.3 | 812.7678 34125.66 2.869513
x = 1 | f(x) = 34824.78 | 779.576 34042.26 2.935698
x = 0.381966 | f(x) = 34880.03 | 788.1485 34088.99 2.894439
x = 0.618034 | f(x) = 34858.6 | 784.1171 34071.57 2.91002
x = 0.763932 | f(x) = 34843.88 | 780.8715 34060.09 2.919804
x = 0.854102 | f(x) = 34835.32 | 779.3894 34053.01 2.925896
x = 0.90983 | f(x) = 34830.74 | 779.0445 34048.76 2.929623
====================== step 30/30 ===============================
x = 0 | computing velocities
computing adjoint
saving results
f(x) = 34824.9 | 779.6846 34042.28 2.935698
x = 1 | f(x) = 34721.73 | 773.8226 33944.9 3.012811
x = 0.381966 | f(x) = 34777.78 | 771.9937 34002.82 2.964712
x = 0.618034 | f(x) = 34756.76 | 772.5218 33981.26 2.983082
x = 0.763932 | f(x) = 34743.45 | 772.8096 33967.65 2.994363
x = 0.854102 | f(x) = 34735.33 | 773.2066 33959.12 3.001402
x = 0.90983 | f(x) = 34730.47 | 773.6083 33953.86 3.005763
preparing final solution
computing new velocity
write lock file:
FemModel initialization elapsed time: 0.134429
Total Core solution elapsed time: 97.4304
Linear solver elapsed time: 58.3618 (60%)
Total elapsed time: 0 hrs 1 min 37 sec
loading results from cluster
Step 4: Transient run
checking model consistency
marshalling file /Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-19-39-57804/SeaRISEgreenland.bin
launching solution sequence
───────────────────────────────────────────────────────────────────
Ice-sheet and Sea-level System Model (ISSM) version 2026.2
GitHub: https://github.com/ISSMteam/ISSM/
Documentation: https://issmteam.github.io/ISSM-Documentation/
───────────────────────────────────────────────────────────────────
Input updates from constant
Input updates from constant
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
Renumbering degrees of freedom
call computational core:
Updating Mmes
iteration 1/100 time [yr]: 0.20 (time step: 0.20)
computing smb
computing new velocity
Updating constraints and active domain of analysis StressbalanceAnalysis for time: 0.2
Get solution from inputs
Reduce vector from g to f set
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.05155e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 41.3709 > 1 %
Convergence criterion: norm(du)/norm(u) 63.1692 > 10 %
Convergence criterion: max(du) 0.000157031
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.08287e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 3.67351 > 1 %
Convergence criterion: norm(du)/norm(u) 7.15747 < 10 %
Convergence criterion: max(du) 8.86618e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.21945e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 1.10917 > 1 %
Convergence criterion: norm(du)/norm(u) 2.86495 < 10 %
Convergence criterion: max(du) 5.14918e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
Allocating matrices (Kff stiffness matrix size: 7398 x 7398)
Assembling matrices
Create nodal constraints
Dirichlet lifting applied to load vector
Solving matrix system
solver residue: norm(KU-F)/norm(F)=2.01372e-16
Merging solution vector from fset to gset
checking convergence
mechanical equilibrium convergence criterion 0.445157 < 1 %
Convergence criterion: norm(du)/norm(u) 1.23492 < 10 %
Convergence criterion: max(du) 2.12087e-06
Input updates from constant
Updating inputs from solution for StressbalanceAnalysis
number of unstable constraints: 0
total number of iterations: 4
computing basal mass balance
computing mass transport
Updating constraints and active domain of analysis MasstransportAnalysis for time: 0.2
Allocating matrices
[1] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[1] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
(Kff stiffness matrix size: 3699 x 3699)
Assembling matrices
[0] ??? Error using ==> ./analyses/MasstransportAnalysis.cpp:720
[0] CreatePVectorCG error message: Assertion "connectedtoocean_input" failed, please report bug at https://github.com/ISSMteam/ISSM/
loading results from cluster
[Warning: Could not copy
/Users/jenkins/workspace/macOS-Intel-Examples//execution/SeaRISEgreenland-06-30-2026-05-19-39-57804//SeaRISEgreenland.outbin]
[> In issmscpin (line 22)
In generic/Download (line 328)
In loadresultsfromcluster (line 45)
In solve (line 210)
In runme (line 111)]
Error using loadresultsfromdisk
=========================================================================
Binary file SeaRISEgreenland.outbin not found
This typically results from an error encountered during the simulation
Please check for error messages above or in the outlog
=========================================================================
Error in loadresultsfromcluster (line 48)
md=loadresultsfromdisk(md,d.miscellaneous.name '.outbin']);
Error in solve (line 210)
md=loadresultsfromcluster(md);
Error in runme (line 111)
md=solve(md,'Transient');FAILURE
finished: Greenland
-----------End of matlab_log.log-----------
Build step 'Execute shell' marked build as failure
Recording test results
Finished: FAILURE
