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Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171018121453)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -8.58453759467e-12. Allowing negative dual variable(s) as small as -1.60452380549e-12. Allowing negative dual variable(s) as small as -1.51414601343e-12. Allowing negative dual variable(s) as small as -3.06575988554e-12. Solving took 4 GP solves and 1.26 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -9.59190582864e-12. Allowing negative dual variable(s) as small as -1.60494881274e-12. Allowing negative dual variable(s) as small as -1.68638974313e-12. Allowing negative dual variable(s) as small as -1.62411837451e-12. Solving took 4 GP solves and 1.76 seconds. Allowing negative dual variable(s) as small as -7.73032332591e-12. Allowing negative dual variable(s) as small as -3.41869518805e-11. Allowing negative dual variable(s) as small as -2.09107453575e-11. Allowing negative dual variable(s) as small as -2.11244563508e-11. Allowing negative dual variable(s) as small as -2.13748393985e-11. Allowing negative dual variable(s) as small as -4.8939186037e-12. Allowing negative dual variable(s) as small as -1.04706166697e-11. Allowing negative dual variable(s) as small as -5.89374404315e-12. Allowing negative dual variable(s) as small as -1.10740710222e-11. MTOW [lbs] = 141.59 Zero fuel weight [lbs] = 53.63 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.77766525059e-12. Allowing negative dual variable(s) as small as -7.11231355928e-12. Allowing negative dual variable(s) as small as -1.34959171659e-11. Allowing negative dual variable(s) as small as -1.37365098679e-11. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.4247659949e-11. Allowing negative dual variable(s) as small as -3.57353853974e-11. Allowing negative dual variable(s) as small as -3.96848167502e-13. Allowing negative dual variable(s) as small as -5.6703124059e-11. Solving took 4 GP solves and 5.25 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.09465863993e-13. Allowing negative dual variable(s) as small as -1.80527866961e-11. Allowing negative dual variable(s) as small as -7.28679586288e-11. Allowing negative dual variable(s) as small as -1.43010061258e-11. Solving took 4 GP solves and 3.59 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -7.73128783216e-12. Allowing negative dual variable(s) as small as -3.42129588549e-11. Allowing negative dual variable(s) as small as -2.08890058029e-11. Allowing negative dual variable(s) as small as -2.11343442746e-11. Allowing negative dual variable(s) as small as -2.14061199322e-11. Allowing negative dual variable(s) as small as -4.88838873894e-12. Allowing negative dual variable(s) as small as -1.04705985635e-11. Allowing negative dual variable(s) as small as -5.89506536034e-12. Allowing negative dual variable(s) as small as -1.10746005465e-11. MTOW [lbs] = 141.59 Zero fuel weight [lbs] = 53.63 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.73444786779e-12. Allowing negative dual variable(s) as small as -7.11344991158e-12. Allowing negative dual variable(s) as small as -1.34977802589e-11. Allowing negative dual variable(s) as small as -1.37369818212e-11. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.42491858043e-11. Allowing negative dual variable(s) as small as -3.57334004698e-11. Allowing negative dual variable(s) as small as -3.97338491582e-13. Allowing negative dual variable(s) as small as -5.67039466512e-11. Solving took 4 GP solves and 1.91 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.09697883258e-13. Allowing negative dual variable(s) as small as -1.8054350983e-11. Allowing negative dual variable(s) as small as -7.28766452567e-11. Allowing negative dual variable(s) as small as -1.43004544838e-11. Solving took 4 GP solves and 1.57 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531