Failed
gpkit.tests.from_paths.TestFiles.test_solar_npod_trade_py_mosek (from gpkit.tests.from_paths.TestFiles-20180501110031)
Failing for the past 1 build
(Since Failed
)
Error Message
The constraint rho_FoamHD/Relax >= 1 is infeasible by 2677.777778%
Stacktrace
Traceback (most recent call last): File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/tests/from_paths.py", line 39, in test_fn mod.test() File "npod_trade.py", line 81, in test File "npod_trade.py", line 26, in pods File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/constraints/prog_factories.py", line 122, in solvefn self.program, progsolve = genfunction(self) File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/constraints/prog_factories.py", line 79, in programify prog = program(self.cost, self, constants, **kwargs) File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/constraints/sgp.py", line 64, in __init__ self._gp = self.init_gp(self.substitutions) File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/constraints/sgp.py", line 186, in init_gp gp = GeometricProgram(self.cost, [gpconstrs, spapproxs], substitutions) File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/constraints/gp.py", line 72, in __init__ self.posynomials.extend(self.as_posyslt1(self.substitutions)) File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/constraints/set.py", line 264, in as_posyslt1 posys = constraint.as_posyslt1(substitutions) File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/constraints/set.py", line 264, in as_posyslt1 posys = constraint.as_posyslt1(substitutions) File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/nomials/math.py", line 498, in as_posyslt1 hmap = self._simplify_posy_ineq(hmap, self.pmap) File "/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/gpkit/gpkit/nomials/math.py", line 442, in _simplify_posy_ineq " %f%%" % (self, -coeff*100)) ValueError: The constraint rho_FoamHD/Relax >= 1 is infeasible by 2677.777778%
Standard Output
Beginning signomial solve. Solving took 9 GP solves and 5.65 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 0.9740 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1359978.9642 but bound is 600000.0000 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1118578.9967 but bound is 1000000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 89126.6215 but bound is 50000.0000 Beginning signomial solve. Beginning signomial solve. Solving took 9 GP solves and 5.46 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 0.9740 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1359978.9643 but bound is 600000.0000 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1118578.9968 but bound is 1000000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 89126.6215 but bound is 50000.0000 Beginning signomial solve. Using solver 'mosek' Solving for 14852 variables. Solving took 4.35 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.3227 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 671709.7359 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.67 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2812 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 729183.6153 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 3.47 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2258 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 802959.5990 but bound is 600000.0000 Using solver 'mosek' Solving for 7672 variables. Solving took 1.73 seconds. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.2008 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 839122.5080 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 4.45 seconds. Allowing negative dual variable(s) as small as -3.906440278640393e-13. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.3227 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 671709.7492 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 4.03 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2812 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 729183.6153 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 3.18 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2258 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 802959.5990 but bound is 600000.0000 Using solver 'mosek' Solving for 7672 variables. Solving took 2.42 seconds. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.2008 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 839122.5081 but bound is 600000.0000 Beginning signomial solve. Solving took 9 GP solves and 3.39 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0930 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1365008.4000 but bound is 600000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 80513.9534 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 3.11544275077 meter ** 2 / second ** 2 but the right hand side evaluated to 3.11543947881 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.27606821662 meter ** 2 / second ** 2 but the right hand side evaluated to 2.27606474066 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00015%) Beginning signomial solve. Solving took 9 GP solves and 3.3 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.0930 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1365008.4187 but bound is 600000.0000 Warning: Variable [Re_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,), Re_Mis could cause inaccurate result because it is below lower bound. Solution is 80513.9534 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(0,)**...] is not tight because the left hand side evaluated to 3.11544275134 meter ** 2 / second ** 2 but the right hand side evaluated to 3.11543947938 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [0.151*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**-2... >= 0.00633*B_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/BladeElementProp/BladeElementPerf_(1,)**...] is not tight because the left hand side evaluated to 2.2760682167 meter ** 2 / second ** 2 but the right hand side evaluated to 2.27606474073 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00015%)
Standard Error
/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) /Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun)