Failed
gpkit.tests.from_paths.TestFiles.test_solar_season_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20200714173615)
Failing for the past 1 build
(Since Failed
)
Error Message
Cannot convert from '1 meter * newton * revolutions_per_minute / volt' to '1 attometer_per_second'
Stacktrace
Traceback (most recent call last): File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/nomials/map.py", line 59, in __add__ other *= float(other.units/self.units) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/venv2_gpkit/lib/python3.7/site-packages/pint/quantity.py", line 788, in __float__ raise DimensionalityError(self._units, "dimensionless") pint.errors.DimensionalityError: Cannot convert from 'attometer_per_second * volt / meter / newton / revolutions_per_minute' 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 59, 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 48, 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 37, in test_fn mod.test() File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/solar/solar/season.py", line 60, in test _ = season(lats=[20], days=[355]) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/solar/solar/season.py", line 21, 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 54, 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 54, 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 54, 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 54, 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 36, in setup i >= Q*Kv+i0, File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/nomials/array.py", line 69, in __add__ out = (np.ndarray.__add__(self, other)) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/nomials/math.py", line 194, in __add__ out = Signomial(self.hmap + other_hmap) File "/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/nomials/map.py", line 61, in __add__ raise DimensionalityError(self.units, other.units) pint.errors.DimensionalityError: Cannot convert from '1 meter * newton * revolutions_per_minute / volt' to '1 attometer_per_second'
Standard Output
N=1 Infeasible monomial equality: Cannot convert from 'Mission.Climb.AircraftDrag.MotorPerf.v[0]·Mission.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]' Infeasible monomial equality: Cannot convert from 'Mission.Climb.AircraftDrag.MotorPerf.v[0]·Mission.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]' Infeasible monomial equality: Cannot convert from 'Mission.Climb.AircraftDrag.MotorPerf.v[1]·Mission.Climb.AircraftDrag.MotorPerf.i[1] [V·amps]' to 'Mission.Climb.AircraftDrag.MotorPerf.Pelec[1] [kW]' Infeasible monomial equality: Cannot convert from 'Mission.Climb.AircraftDrag.MotorPerf.v[2]·Mission.Climb.AircraftDrag.MotorPerf.i[2] [V·amps]' to 'Mission.Climb.AircraftDrag.MotorPerf.Pelec[2] [kW]' Infeasible monomial equality: Cannot convert from 'Mission.Climb.AircraftDrag.MotorPerf.v[3]·Mission.Climb.AircraftDrag.MotorPerf.i[3] [V·amps]' to 'Mission.Climb.AircraftDrag.MotorPerf.Pelec[3] [kW]' Infeasible monomial equality: Cannot convert from 'Mission.Climb.AircraftDrag.MotorPerf.v[4]·Mission.Climb.AircraftDrag.MotorPerf.i[4] [V·amps]' to 'Mission.Climb.AircraftDrag.MotorPerf.Pelec[4] [kW]' N=1 Infeasible monomial equality: Cannot convert from 'Mission1.Climb.AircraftDrag.MotorPerf.v[0]·Mission1.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission1.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]' Infeasible monomial equality: Cannot convert from 'Mission1.Climb.AircraftDrag.MotorPerf.v[0]·Mission1.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission1.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]' Infeasible monomial equality: Cannot convert from 'Mission1.Climb.AircraftDrag.MotorPerf.v[1]·Mission1.Climb.AircraftDrag.MotorPerf.i[1] [V·amps]' to 'Mission1.Climb.AircraftDrag.MotorPerf.Pelec[1] [kW]' Infeasible monomial equality: Cannot convert from 'Mission1.Climb.AircraftDrag.MotorPerf.v[2]·Mission1.Climb.AircraftDrag.MotorPerf.i[2] [V·amps]' to 'Mission1.Climb.AircraftDrag.MotorPerf.Pelec[2] [kW]' Infeasible monomial equality: Cannot convert from 'Mission1.Climb.AircraftDrag.MotorPerf.v[3]·Mission1.Climb.AircraftDrag.MotorPerf.i[3] [V·amps]' to 'Mission1.Climb.AircraftDrag.MotorPerf.Pelec[3] [kW]' Infeasible monomial equality: Cannot convert from 'Mission1.Climb.AircraftDrag.MotorPerf.v[4]·Mission1.Climb.AircraftDrag.MotorPerf.i[4] [V·amps]' to 'Mission1.Climb.AircraftDrag.MotorPerf.Pelec[4] [kW]' Infeasible monomial equality: Cannot convert from 'Mission2.Climb.AircraftDrag.MotorPerf.v[0]·Mission2.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission2.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]' Infeasible monomial equality: Cannot convert from 'Mission2.Climb.AircraftDrag.MotorPerf.v[0]·Mission2.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission2.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]' Infeasible monomial equality: Cannot convert from 'Mission2.Climb.AircraftDrag.MotorPerf.v[1]·Mission2.Climb.AircraftDrag.MotorPerf.i[1] [V·amps]' to 'Mission2.Climb.AircraftDrag.MotorPerf.Pelec[1] [kW]' Infeasible monomial equality: Cannot convert from 'Mission2.Climb.AircraftDrag.MotorPerf.v[2]·Mission2.Climb.AircraftDrag.MotorPerf.i[2] [V·amps]' to 'Mission2.Climb.AircraftDrag.MotorPerf.Pelec[2] [kW]' Infeasible monomial equality: Cannot convert from 'Mission2.Climb.AircraftDrag.MotorPerf.v[3]·Mission2.Climb.AircraftDrag.MotorPerf.i[3] [V·amps]' to 'Mission2.Climb.AircraftDrag.MotorPerf.Pelec[3] [kW]' Infeasible monomial equality: Cannot convert from 'Mission2.Climb.AircraftDrag.MotorPerf.v[4]·Mission2.Climb.AircraftDrag.MotorPerf.i[4] [V·amps]' to 'Mission2.Climb.AircraftDrag.MotorPerf.Pelec[4] [kW]' Infeasible monomial equality: 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]' Infeasible monomial equality: 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]' Infeasible monomial equality: Cannot convert from 'Mission3.Climb.AircraftDrag.MotorPerf.v[1]·Mission3.Climb.AircraftDrag.MotorPerf.i[1] [V·amps]' to 'Mission3.Climb.AircraftDrag.MotorPerf.Pelec[1] [kW]' Infeasible monomial equality: Cannot convert from 'Mission3.Climb.AircraftDrag.MotorPerf.v[2]·Mission3.Climb.AircraftDrag.MotorPerf.i[2] [V·amps]' to 'Mission3.Climb.AircraftDrag.MotorPerf.Pelec[2] [kW]' Infeasible monomial equality: Cannot convert from 'Mission3.Climb.AircraftDrag.MotorPerf.v[3]·Mission3.Climb.AircraftDrag.MotorPerf.i[3] [V·amps]' to 'Mission3.Climb.AircraftDrag.MotorPerf.Pelec[3] [kW]' Infeasible monomial equality: Cannot convert from 'Mission3.Climb.AircraftDrag.MotorPerf.v[4]·Mission3.Climb.AircraftDrag.MotorPerf.i[4] [V·amps]' to 'Mission3.Climb.AircraftDrag.MotorPerf.Pelec[4] [kW]' Infeasible monomial equality: 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]' Infeasible monomial equality: 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]' Infeasible monomial equality: Cannot convert from 'Mission4.Climb.AircraftDrag.MotorPerf.v[1]·Mission4.Climb.AircraftDrag.MotorPerf.i[1] [V·amps]' to 'Mission4.Climb.AircraftDrag.MotorPerf.Pelec[1] [kW]' Infeasible monomial equality: Cannot convert from 'Mission4.Climb.AircraftDrag.MotorPerf.v[2]·Mission4.Climb.AircraftDrag.MotorPerf.i[2] [V·amps]' to 'Mission4.Climb.AircraftDrag.MotorPerf.Pelec[2] [kW]' Infeasible monomial equality: Cannot convert from 'Mission4.Climb.AircraftDrag.MotorPerf.v[3]·Mission4.Climb.AircraftDrag.MotorPerf.i[3] [V·amps]' to 'Mission4.Climb.AircraftDrag.MotorPerf.Pelec[3] [kW]' Infeasible monomial equality: Cannot convert from 'Mission4.Climb.AircraftDrag.MotorPerf.v[4]·Mission4.Climb.AircraftDrag.MotorPerf.i[4] [V·amps]' to 'Mission4.Climb.AircraftDrag.MotorPerf.Pelec[4] [kW]' Infeasible monomial equality: Cannot convert from 'Mission5.Climb.AircraftDrag.MotorPerf.v[0]·Mission5.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission5.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]' Infeasible monomial equality: Cannot convert from 'Mission5.Climb.AircraftDrag.MotorPerf.v[0]·Mission5.Climb.AircraftDrag.MotorPerf.i[0] [V·amps]' to 'Mission5.Climb.AircraftDrag.MotorPerf.Pelec[0] [kW]' Infeasible monomial equality: Cannot convert from 'Mission5.Climb.AircraftDrag.MotorPerf.v[1]·Mission5.Climb.AircraftDrag.MotorPerf.i[1] [V·amps]' to 'Mission5.Climb.AircraftDrag.MotorPerf.Pelec[1] [kW]' Infeasible monomial equality: Cannot convert from 'Mission5.Climb.AircraftDrag.MotorPerf.v[2]·Mission5.Climb.AircraftDrag.MotorPerf.i[2] [V·amps]' to 'Mission5.Climb.AircraftDrag.MotorPerf.Pelec[2] [kW]' Infeasible monomial equality: Cannot convert from 'Mission5.Climb.AircraftDrag.MotorPerf.v[3]·Mission5.Climb.AircraftDrag.MotorPerf.i[3] [V·amps]' to 'Mission5.Climb.AircraftDrag.MotorPerf.Pelec[3] [kW]' Infeasible monomial equality: Cannot convert from 'Mission5.Climb.AircraftDrag.MotorPerf.v[4]·Mission5.Climb.AircraftDrag.MotorPerf.i[4] [V·amps]' to 'Mission5.Climb.AircraftDrag.MotorPerf.Pelec[4] [kW]'
Standard Error
/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/venv2_gpkit/lib/python3.7/site-packages/gpfit/fit_constraintset.py:46: VisibleDeprecationWarning: Creating an ndarray from ragged nested sequences (which is a list-or-tuple of lists-or-tuples-or ndarrays with different lengths or shapes) is deprecated. If you meant to do this, you must specify 'dtype=object' when creating the ndarray for k in range(fitdata["K"])] /Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/venv2_gpkit/lib/python3.7/site-packages/numpy/core/_asarray.py:83: VisibleDeprecationWarning: Creating an ndarray from ragged nested sequences (which is a list-or-tuple of lists-or-tuples-or ndarrays with different lengths or shapes) is deprecated. If you meant to do this, you must specify 'dtype=object' when creating the ndarray return array(a, dtype, copy=False, order=order)