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gpkit.tests.from_paths.TestFiles.test_solar_solar_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171218112913)

Failing for the past 1 build (Since Failed #63 )
Took 9.3 sec.

Error Message

setup() takes exactly 4 arguments (5 given)

Stacktrace

Traceback (most recent call last):
  File "/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn
    mod.test()
  File "solar.py", line 486, in test
  File "/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
  File "solar.py", line 467, in setup
  File "/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
  File "solar.py", line 85, in setup
  File "/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/constraints/model.py", line 59, in __init__
    cs = self.setup(*args, **kwargs)  # pylint: disable=no-member
TypeError: setup() takes exactly 4 arguments (5 given)
		

Standard Output

Using solver 'mosek'
Solving for 5670 variables.
Solving took 1.59 seconds.
Warning: Variable Re_Mission/FlightSegment.38/AircraftPerf.38/WingAero.38 could cause inaccurate result because it is below lower bound. Solution is 120042.1846 but bound is 125000.0000
Warning: Variable Re_Mission/FlightSegment.39/AircraftPerf.39/WingAero.39 could cause inaccurate result because it is below lower bound. Solution is 121471.1981 but bound is 125000.0000
Using solver 'mosek'
Solving for 5670 variables.
Solving took 1.19 seconds.
Warning: Variable Re_Mission.1/FlightSegment.78/AircraftPerf.78/WingAero.78 could cause inaccurate result because it is below lower bound. Solution is 122823.1089 but bound is 125000.0000
Warning: Variable Re_Mission.1/FlightSegment.79/AircraftPerf.79/WingAero.79 could cause inaccurate result because it is below lower bound. Solution is 123244.6837 but bound is 125000.0000
Using solver 'mosek'
Solving for 5670 variables.
Solving took 0.909 seconds.
Using solver 'mosek'
Solving for 2910 variables.
Solving took 0.482 seconds.
Using solver 'mosek'
Solving for 5670 variables.
Solving took 1.07 seconds.
Warning: Variable Re_Mission/FlightSegment.38/AircraftPerf.38/WingAero.38 could cause inaccurate result because it is below lower bound. Solution is 120042.1845 but bound is 125000.0000
Warning: Variable Re_Mission/FlightSegment.39/AircraftPerf.39/WingAero.39 could cause inaccurate result because it is below lower bound. Solution is 121471.1971 but bound is 125000.0000
Using solver 'mosek'
Solving for 5670 variables.
Solving took 1.21 seconds.
Warning: Variable Re_Mission.1/FlightSegment.78/AircraftPerf.78/WingAero.78 could cause inaccurate result because it is below lower bound. Solution is 122823.1089 but bound is 125000.0000
Warning: Variable Re_Mission.1/FlightSegment.79/AircraftPerf.79/WingAero.79 could cause inaccurate result because it is below lower bound. Solution is 123244.6837 but bound is 125000.0000
Using solver 'mosek'
Solving for 5670 variables.
Solving took 0.917 seconds.
Using solver 'mosek'
Solving for 2910 variables.
Solving took 0.452 seconds.
Using solver 'mosek'
Solving for 288 variables.
Solving took 0.145 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 122179.8905 but bound is 125000.0000
Using solver 'mosek'
Solving for 288 variables.
Solving took 0.15 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 122179.8905 but bound is 125000.0000
Using solver 'mosek'
Solving for 2910 variables.
Solving took 0.424 seconds.
Using solver 'mosek_cli'
Solving for 2910 variables.
Solving took 0.71 seconds.
	

Standard Error

/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
/jenkins/workspace/gplibrary_PR_Models/buildnode/reynolds/optimizer/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
  tau = np.exp(-0.175/costhsun)