Passed

gpkit.tests.from_paths.TestFiles.test_solar_npod_trade_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180428171626)

Took 6.6 sec.

Standard Output

Beginning signomial solve.
Solving took 9 GP solves and 4.32 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 1388463.4297 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 1248776.6475 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 82150.9619 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 2.2964550408 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645197474 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)

Beginning signomial solve.
Solving took 9 GP solves and 4.34 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 1388463.4787 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 1248776.6917 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 82150.9619 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 2.29645504556 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645197951 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)

Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.92 seconds.
Allowing negative dual variable(s) as small as -4.390308321909989e-12.
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 765970.5112 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.67 seconds.
Allowing negative dual variable(s) as small as -2.6754100534609902e-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 862671.9754 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.65 seconds.
Allowing negative dual variable(s) as small as -4.2507134352200836e-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 987087.3039 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 1.28 seconds.
Allowing negative dual variable(s) as small as -5.1872096589028224e-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 1058302.4651 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.74 seconds.
Allowing negative dual variable(s) as small as -6.755196001822808e-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 765970.5366 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 3.18 seconds.
Allowing negative dual variable(s) as small as -5.1317169735913295e-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 862671.9863 but bound is 600000.0000
Using solver 'mosek'
Solving for 12129 variables.
Solving took 2.46 seconds.
Allowing negative dual variable(s) as small as -6.539248666405341e-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 987087.2964 but bound is 600000.0000
Using solver 'mosek'
Solving for 6269 variables.
Solving took 1.01 seconds.
Allowing negative dual variable(s) as small as -1.5561912078688723e-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 1058302.4687 but bound is 600000.0000
Beginning signomial solve.
Solving took 9 GP solves and 5.18 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 1388463.8583 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 1248777.0335 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 2.29645503819 meter ** 2 / second ** 2 but the right hand side evaluated to 2.29645197214 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)

Beginning signomial solve.
Solving took 9 GP solves and 2.65 seconds.
Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 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 1388463.8652 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 1248777.0397 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 2.2964550321 meter ** 2 / second ** 2 but the right hand side evaluated to 2.2964519661 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00013%)

Using solver 'mosek'
Solving for 702 variables.
Solving took 0.128 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 838075.6385 but bound is 600000.0000
Beginning signomial solve.
Solving took 8 GP solves and 2.49 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 1017213.8535 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 78650.4124 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 2.62125874995 meter ** 2 / second ** 2 but the right hand side evaluated to 2.62124739897 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 1.95293541995 meter ** 2 / second ** 2 but the right hand side evaluated to 1.95292215072 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 1.04275941384 meter ** 2 / second ** 2 but the right hand side evaluated to 1.04275521475 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 0.467698132658 meter ** 2 / second ** 2 but the right hand side evaluated to 0.467697002309 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 0.139006791301 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006573144 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00016%)

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.5352700378000323e-08.
Solving took 10 GP solves and 3.13 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 882486.3930 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 2.6817616385 force_pound but the right hand side evaluated to 2.68175718428 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 72.1672193391 meter * revolutions_per_minute but the right hand side evaluated to 7.06168158676 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 0.547 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 4.39 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 2.62125876682 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 0.139006754739 meter ** 2 / second ** 2 but the right hand side evaluated to 0.139006562766 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00014%)

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.535278e-08.
Solving took 10 GP solves and 5.51 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 2.68176167677 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 7.06168392103 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

/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
/Users/jenkins/workspace/gpkit_ResearchModel_solar_PR/mosek/venv2_gpkit/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
  tau = np.exp(-0.175/costhsun)