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Passed
gpkit.tests.from_paths.TestFiles.test_solar_season_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428201823)
Standard Output
Beginning signomial solve. Solving took 9 GP solves and 7.38 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 1388463.4681 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 1248776.6823 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 82150.9617 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 2.29645503679 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645197069 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Beginning signomial solve. Solving took 9 GP solves and 6.43 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 1.0624 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 1388463.3836 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 1248776.6063 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 82150.9617 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 2.29645503101 meter ** 2 / second ** 2 but the right hand side evaluated to 2.2964519649 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Using solver 'mosek' Solving for 12129 variables. Solving took 4.61 seconds. Allowing negative dual variable(s) as small as -3.829697667708383e-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 765970.5256 but bound is 600000.0000 Using solver 'mosek' Solving for 12129 variables. Solving took 3.64 seconds. Allowing negative dual variable(s) as small as -3.975947596917721e-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 862671.9794 but bound is 600000.0000 Using solver 'mosek' Solving for 12129 variables. Solving took 5.03 seconds. Allowing negative dual variable(s) as small as -7.438332178501111e-12. 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 987087.2969 but bound is 600000.0000 Using solver 'mosek' Solving for 6269 variables. Solving took 1.51 seconds. Allowing negative dual variable(s) as small as -9.84779369428561e-12. 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 1058302.4652 but bound is 600000.0000 Using solver 'mosek' Solving for 12129 variables. Solving took 4.15 seconds. Allowing negative dual variable(s) as small as -2.929052414286166e-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 765970.5413 but bound is 600000.0000 Using solver 'mosek' Solving for 12129 variables. Solving took 3.88 seconds. Allowing negative dual variable(s) as small as -2.7060362837447194e-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 862671.9749 but bound is 600000.0000 Using solver 'mosek' Solving for 12129 variables. Solving took 5.08 seconds. Allowing negative dual variable(s) as small as -1.3443095298342113e-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 987087.2997 but bound is 600000.0000 Using solver 'mosek' Solving for 6269 variables. Solving took 1.66 seconds. Allowing negative dual variable(s) as small as -2.7223571228268817e-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 1058302.4637 but bound is 600000.0000 Beginning signomial solve. Solving took 9 GP solves and 6.87 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 1388463.4898 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 1248776.7018 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 82150.9618 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 2.29645503644 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645197038 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Beginning signomial solve. Solving took 9 GP solves and 8.09 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 1388472.0070 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 1248784.3706 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 82150.9591 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 2.2964551412 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645207528 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%) Using solver 'mosek' Solving for 702 variables. Solving took 0.356 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 838075.6768 but bound is 600000.0000 Beginning signomial solve. Solving took 8 GP solves and 5.67 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 1017213.8323 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 78650.4127 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 2.62125873782 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124738696 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 1.95293541712 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292214802 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 1.04275941597 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521691 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 0.467698134544 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697004206 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 0.139006792062 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006573907 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%) Beginning signomial solve. Allowing negative dual variable(s) as small as -1.5352780195207032e-08. Solving took 10 GP solves and 7.39 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.4/WingAero.4_(0,), CL_Mission.2/Climb.2/AircraftDrag.4/WingAero.4 could cause inaccurate result because it is below lower bound. Solution is 1.2129 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.4/WingAero.4_(0,), Re_Mission.2/Climb.2/AircraftDrag.4/WingAero.4 could cause inaccurate result because it is above upper bound. Solution is 882486.4030 but bound is 600000.0000 Warning: Constraint [dT_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1/BladeElementPerf.1_(0,... >= T_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1 [lbf]...] is not tight because the left hand side evaluated to 2.68176163805 force_pound but the right hand side evaluated to 2.68175718382 force_pound (Allowable error: 0.0001%, Actual error: 0.00017%) Warning: Constraint [omega_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1/BladeElementPerf.1_... >= Wt_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1/BladeElementPerf.1_(0,...] is not tight because the left hand side evaluated to 72.1672194077 meter * revolutions_per_minute but the right hand side evaluated to 7.06168153356 meter / second (Allowable error: 0.0001%, Actual error: 7%) Warning: Variable [Re_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1/BladeElementPerf.1_(0 could cause inaccurate result because it is below lower bound. Solution is 82590.0950 but bound is 50000.0000 Using solver 'mosek_cli' Solving for 702 variables. Solving took 0.719 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 Beginning signomial solve. Solving took 8 GP solves and 12.6 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 0.467698068221 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%) Beginning signomial solve. Allowing negative dual variable(s) as small as -1.535278e-08. Solving took 10 GP solves and 45.5 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.4/WingAero.4_(0,), CL_Mission.2/Climb.2/AircraftDrag.4/WingAero.4 could cause inaccurate result because it is below lower bound. Solution is 1.2129 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.4/WingAero.4_(0,), Re_Mission.2/Climb.2/AircraftDrag.4/WingAero.4 could cause inaccurate result because it is above upper bound. Solution is 882487.5853 but bound is 600000.0000 Warning: Constraint [dT_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1/BladeElementPerf.1_(0,... >= T_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1 [lbf]...] is not tight because the left hand side evaluated to 2.68176164062 force_pound but the right hand side evaluated to 2.68175706241 force_pound (Allowable error: 0.0001%, Actual error: 0.00017%) Warning: Constraint [omega_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1/BladeElementPerf.1_... >= Wt_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1/BladeElementPerf.1_(0,...] is not tight because the left hand side evaluated to 72.1672253273 meter * revolutions_per_minute but the right hand side evaluated to 7.06168317666 meter / second (Allowable error: 0.0001%, Actual error: 7%) Warning: Variable [Re_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1/BladeElementPerf.1_(0 could cause inaccurate result because it is below lower bound. Solution is 82590.5049 but bound is 50000.0000 Warning: Constraint [-B_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1/BladeElementPerf.1_(4,... >= dT_Mission.2/FlightSegment.2/AircraftPerf.2/AircraftDrag.5/BladeElementProp.1/BladeElementPerf.1_(4,...] is not tight because the left hand side evaluated to 3.56206132463 kilogram * meter / second ** 2 but the right hand side evaluated to 0.800784105063 force_pound (Allowable error: 0.0001%, Actual error: 0.00011%)
Standard Error
C:\Users\jenkins\workspace\gpkit_ResearchModel_solar_PR\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\gpkit_ResearchModel_solar_PR\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)