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gpkit.tests.from_paths.TestFiles.test_solar_sens_chart_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20200302155331)

Failing for the past 1 build (Since Failed #214 )
Took 0.25 sec.

Error Message

Cannot convert from 'Mission4.Climb.AircraftDrag.MotorPerf.v[0]*Mission4.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission4.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/sens_chart.py", line 95, in test
    model = Mission(v, latitude=[20])
  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 'Mission4.Climb.AircraftDrag.MotorPerf.v[0]*Mission4.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission4.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]'

Standard Output


N=1

N=1

Standard Error