Failed
gpkit.tests.from_paths.TestFiles.test_solar_season_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20200302155331)
Failing for the past 1 build
(Since Failed
)
Error Message
Cannot convert from 'Mission3.Climb.AircraftDrag.MotorPerf.v[0]*Mission3.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission3.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]'
Stacktrace
Traceback (most recent call last): File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/_pint/__init__.py", line 53, in of_division self.division_cache[key] = float(conversion) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/venv2_gpkit/lib/python3.7/site-packages/pint/quantity.py", line 756, in __float__ raise DimensionalityError(self._units, "dimensionless") pint.errors.DimensionalityError: Cannot convert from 'attometer_per_second * volt / kilowatt' to 'dimensionless' During handling of the above exception, another exception occurred: Traceback (most recent call last): File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/tests/from_paths.py", line 40, in test_fn mod.test() File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/solar/solar/season.py", line 62, in test _ = season([20]) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/solar/solar/season.py", line 23, in season M = Mission(V, latitude=range(1, l+1, 1), day=d) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/model.py", line 56, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/solar/solar/solar.py", line 648, in setup self.mission.append(Climb(5, self.aircraft)) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/model.py", line 56, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/solar/solar/solar.py", line 605, in setup self.drag = AircraftDrag(aircraft, self) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/model.py", line 56, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/solar/solar/solar.py", line 92, in setup self.motor = static.motor.flight_model(static.motor, state) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/model.py", line 56, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkitmodels/GP/aircraft/motor/motor.py", line 32, in setup Pelec == v*i, File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/nomials/array.py", line 45, in wrapped_func result = vecfunc(left, right) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/venv2_gpkit/lib/python3.7/site-packages/numpy/lib/function_base.py", line 2091, in __call__ return self._vectorize_call(func=func, args=vargs) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/venv2_gpkit/lib/python3.7/site-packages/numpy/lib/function_base.py", line 2161, in _vectorize_call ufunc, otypes = self._get_ufunc_and_otypes(func=func, args=args) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/venv2_gpkit/lib/python3.7/site-packages/numpy/lib/function_base.py", line 2121, in _get_ufunc_and_otypes outputs = func(*inputs) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/nomials/math.py", line 348, in __eq__ return MonomialEquality(self, other) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/nomials/math.py", line 556, in __init__ self.unsubbed = self._gen_unsubbed(self.left, self.right) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/nomials/math.py", line 581, in _gen_unsubbed l_over_r = unsubbed(self, left, right) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/nomials/math.py", line 485, in _gen_unsubbed m_c *= units.of_division(m_gt, p_lt) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/_pint/__init__.py", line 55, in of_division raise DimensionalityError(numerator, denominator) pint.errors.DimensionalityError: Cannot convert from 'Mission3.Climb.AircraftDrag.MotorPerf.v[0]*Mission3.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission3.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]'
Standard Output
N=1 N=1