Failed
gpkit.tests.from_paths.TestFiles.test_solar_solar_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428160504)
Failing for the past 1 build
(Since Failed
)
Error Message
An ArrayConstraint was created with elements of numpy.bool_ Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]
Stacktrace
Traceback (most recent call last): File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\tests\from_paths.py", line 39, in test_fn mod.test() File "solar.py", line 654, in test File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 61, in __init__ cs = self.setup(*args, **kwargs) # pylint: disable=no-member File "solar.py", line 633, in setup File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\model.py", line 83, in __init__ CostedConstraintSet.__init__(self, cost, constraints, substitutions) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\costed.py", line 21, in __init__ ConstraintSet.__init__(self, constraints, subs) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 58, in __init__ list.__setitem__(self, i, ConstraintSet(constraint)) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 67, in __init__ raise_elementhasnumpybools(constraint) File "c:\users\jenkins\workspace\gplibrary_pr_models\mosek\gpkit\gpkit\constraints\set.py", line 357, in raise_elementhasnumpybools % (cause, constraint)) ValueError: An ArrayConstraint was created with elements of numpy.bool_ Full constraint: Sout_Mission.2/FlightSegment.2/SparLoading.6 = [gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Monomial(0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N]), gpkit.Variable(z0_Mission.2/FlightSegment.2 [N])]
Standard Output
Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 9 GP solves and 5.59 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 1.0624 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 1388461.0993 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 1248774.5487 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 82150.9623 but bound is 50000.0000 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 2.29645500327 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645193703 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 9 GP solves and 5.71 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 1.0624 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 1388463.4586 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 1248776.6745 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 82150.9601 but bound is 50000.0000 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 2.29645501839 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645195175 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 5.38 seconds. Allowing negative dual variable(s) as small as -8.19247542299993e-11. 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 1.2510 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 765970.6061 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.65/GustL.65_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.58/GustL.58_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.69/GustL.69_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.46/GustL.46_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.78/GustL.78_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.48/GustL.48_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.52/GustL.52_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.71/GustL.71_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.75/GustL.75_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.59/GustL.59_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.66/GustL.66_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.49/GustL.49_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.67/GustL.67_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.64/GustL.64_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.40/GustL.40_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.55/GustL.55_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.54/GustL.54_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.53/GustL.53_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.60/GustL.60_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.51/GustL.51_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.41/GustL.41_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.47/GustL.47_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.70/GustL.70_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.50/GustL.50_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.74/GustL.74_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.68/GustL.68_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.76/GustL.76_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.79/GustL.79_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.63/GustL.63_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.44/GustL.44_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.77/GustL.77_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.56/GustL.56_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.57/GustL.57_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.42/GustL.42_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.62/GustL.62_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.61/GustL.61_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.45/GustL.45_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.43/GustL.43_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.72/GustL.72_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.73/GustL.73_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 3.48 seconds. Allowing negative dual variable(s) as small as -7.834061262334159e-11. 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 1.1911 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 862671.9975 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.90/GustL.90_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.118/GustL.118_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.119/GustL.119_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.104/GustL.104_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.102/GustL.102_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.93/GustL.93_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.105/GustL.105_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.85/GustL.85_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.106/GustL.106_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.117/GustL.117_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.91/GustL.91_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.109/GustL.109_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.116/GustL.116_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.114/GustL.114_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.96/GustL.96_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.101/GustL.101_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.87/GustL.87_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.100/GustL.100_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.99/GustL.99_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.88/GustL.88_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.98/GustL.98_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.113/GustL.113_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.89/GustL.89_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.81/GustL.81_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.95/GustL.95_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.107/GustL.107_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.94/GustL.94_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.115/GustL.115_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.110/GustL.110_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.84/GustL.84_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.82/GustL.82_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.83/GustL.83_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.97/GustL.97_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.112/GustL.112_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.86/GustL.86_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.92/GustL.92_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.111/GustL.111_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.103/GustL.103_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.108/GustL.108_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.80/GustL.80_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 5.92 seconds. Allowing negative dual variable(s) as small as -2.918435053034562e-11. 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 1.1202 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 987087.3059 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 6269 variables. Solving took 1.8 seconds. Allowing negative dual variable(s) as small as -3.12870574518503e-11. 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 1.0863 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 1058302.4851 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.8/GustL.8_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.10/GustL.10_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.16/GustL.16_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.27/GustL.27_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.39/GustL.39_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.23/GustL.23_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.14/GustL.14_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.4/GustL.4_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.19/GustL.19_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.3/GustL.3_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.13/GustL.13_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.26/GustL.26_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.28/GustL.28_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.18/GustL.18_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.25/GustL.25_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.15/GustL.15_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.29/GustL.29_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.24/GustL.24_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.31/GustL.31_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.9/GustL.9_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.2/GustL.2_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.37/GustL.37_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.6/GustL.6_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.33/GustL.33_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.38/GustL.38_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.35/GustL.35_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.11/GustL.11_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.12/GustL.12_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.34/GustL.34_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.32/GustL.32_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.7/GustL.7_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.36/GustL.36_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.30/GustL.30_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.5/GustL.5_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.20/GustL.20_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.21/GustL.21_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.17/GustL.17_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment.22/GustL.22_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 3.68 seconds. Allowing negative dual variable(s) as small as -1.0471123535107248e-11. 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 1.2510 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 765970.5160 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.65/GustL.65_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.58/GustL.58_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.69/GustL.69_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.46/GustL.46_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.78/GustL.78_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.48/GustL.48_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.52/GustL.52_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.71/GustL.71_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.75/GustL.75_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.59/GustL.59_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.66/GustL.66_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.49/GustL.49_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.67/GustL.67_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.64/GustL.64_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.40/GustL.40_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.55/GustL.55_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.54/GustL.54_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.53/GustL.53_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.60/GustL.60_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.51/GustL.51_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.41/GustL.41_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.47/GustL.47_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.70/GustL.70_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.50/GustL.50_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.74/GustL.74_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.68/GustL.68_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.76/GustL.76_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.79/GustL.79_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.63/GustL.63_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.44/GustL.44_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.77/GustL.77_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.56/GustL.56_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.57/GustL.57_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.42/GustL.42_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.62/GustL.62_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.61/GustL.61_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.45/GustL.45_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.43/GustL.43_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.72/GustL.72_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.73/GustL.73_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 3.63 seconds. Allowing negative dual variable(s) as small as -8.117145612342004e-11. 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 1.1911 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 862671.9978 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.90/GustL.90_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.118/GustL.118_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.119/GustL.119_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.104/GustL.104_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.102/GustL.102_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.93/GustL.93_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.105/GustL.105_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.85/GustL.85_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.106/GustL.106_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.117/GustL.117_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.91/GustL.91_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.109/GustL.109_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.116/GustL.116_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.114/GustL.114_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.96/GustL.96_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.101/GustL.101_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.87/GustL.87_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.100/GustL.100_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.99/GustL.99_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.88/GustL.88_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.98/GustL.98_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.113/GustL.113_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.89/GustL.89_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.81/GustL.81_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.95/GustL.95_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.107/GustL.107_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.94/GustL.94_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.115/GustL.115_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.110/GustL.110_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.84/GustL.84_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.82/GustL.82_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.83/GustL.83_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.97/GustL.97_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.112/GustL.112_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.86/GustL.86_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.92/GustL.92_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.111/GustL.111_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.103/GustL.103_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.108/GustL.108_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.2/FlightSegment.80/GustL.80_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 12129 variables. Solving took 3.38 seconds. Allowing negative dual variable(s) as small as -6.930846963973269e-11. 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 1.1202 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 987087.3138 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.139/GustL.139_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.135/GustL.135_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.136/GustL.136_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.130/GustL.130_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.127/GustL.127_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.131/GustL.131_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.125/GustL.125_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.128/GustL.128_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.132/GustL.132_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.129/GustL.129_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.122/GustL.122_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.121/GustL.121_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.137/GustL.137_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.138/GustL.138_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.123/GustL.123_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.120/GustL.120_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.134/GustL.134_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.124/GustL.124_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.133/GustL.133_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Couldn't auto-differentiate linked variable cosminus1_Mission.3/FlightSegment.126/GustL.126_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 6269 variables. Solving took 1.75 seconds. Allowing negative dual variable(s) as small as -2.0105004462850625e-11. 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 1.0863 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 1058302.4804 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 9 GP solves and 5.11 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 1.0624 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 1388461.1258 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 1248774.5739 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 82150.9608 but bound is 50000.0000 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 2.29645499448 meter ** 2 / second ** 2 but the right hand side evaluated to 2.2964519278 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 9 GP solves and 5.23 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 1.0624 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 1388485.8708 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 1248796.8535 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 82150.9545 but bound is 50000.0000 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 2.29645531221 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645224651 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek' Solving for 702 variables. Solving took 0.422 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 1.1958 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 838075.6769 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 8 GP solves and 4.8 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.1418 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1017215.3805 but bound is 600000.0000 Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,), could cause inaccurate result because it is below lower bound. Solution is 78650.4125 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 2.62125882769 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124747684 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00043%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(1... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.95293542382 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215473 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00068%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.0427594177 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521865 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0004%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(3... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.46769813495 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697004612 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00024%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(4... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.139006791945 meter ** 2 / second ** 2 but the right hand side evaluated to 0.13900657379 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%) Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]' Couldn't auto-differentiate linked variable cosminus1_Mission/FlightSegment/GustL_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Using solver 'mosek_cli' Solving for 702 variables. Solving took 0.43 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 1.1958 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 838072.5912 but bound is 600000.0000 Couldn't auto-differentiate linked variable cosminus1_Mission.1/FlightSegment.1/GustL.1_(0,). (to raise the error directly for debugging purposes, set gpkit.settings["ad_errors_raise"] to True) Beginning signomial solve. Solving took 8 GP solves and 6.01 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.1418 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1017215.9574 but bound is 600000.0000 Warning: Constraint [dQ_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2,) [N... >= B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2,)*G_M...] is not tight because the left hand side evaluated to 0.546199983583 meter * newton but the right hand side evaluated to 0.54619937481 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Variable [Re_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0,), could cause inaccurate result because it is below lower bound. Solution is 78650.5577 but bound is 50000.0000 Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(0... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 2.62125881924 meter ** 2 / second ** 2 but the right hand side evaluated to 2.6212478085 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00042%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(1... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.9529359766 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292347375 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00064%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(2... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 1.04275932764 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275522741 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00039%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(3... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.467698058867 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697044815 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00022%) Warning: Constraint [0.151*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_(4... >= 0.00633*B_Mission.1/FlightSegment.1/AircraftPerf.1/AircraftDrag.3/BladeElementProp/BladeElementPerf_...] is not tight because the left hand side evaluated to 0.13900678254 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006562766 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%) Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/SparLoading.6_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(0,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(1,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(2,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(3,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(4,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(5,)' to '0.2*Nsafety_Mission.2/FlightSegment.2/SparLoading.6*W_Aircraft.2/Battery.2 [lbf]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(6,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(7,)' to 'z0_Mission.2/FlightSegment.2 [N]' Infeasible monomial equality: Cannot convert from 'Sout_Mission.2/FlightSegment.2/GustL.2_(8,)' to 'z0_Mission.2/FlightSegment.2 [N]'
Standard Error
C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) C:\Users\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun)