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Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171025135824)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -1.11822213815e-11. Allowing negative dual variable(s) as small as -1.59897702717e-12. Allowing negative dual variable(s) as small as -1.72772256571e-12. Allowing negative dual variable(s) as small as -1.66390555847e-12. Solving took 4 GP solves and 5.8 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.07512883145e-11. Allowing negative dual variable(s) as small as -1.59868429259e-12. Allowing negative dual variable(s) as small as -2.85500139155e-12. Allowing negative dual variable(s) as small as -1.61883744257e-12. Solving took 4 GP solves and 1.5 seconds. Allowing negative dual variable(s) as small as -7.72320402076e-12. Allowing negative dual variable(s) as small as -3.41912609336e-11. Allowing negative dual variable(s) as small as -2.09051248534e-11. Allowing negative dual variable(s) as small as -2.11102108016e-11. Allowing negative dual variable(s) as small as -2.13599346544e-11. Allowing negative dual variable(s) as small as -4.89104329954e-12. Allowing negative dual variable(s) as small as -1.04719063282e-11. Allowing negative dual variable(s) as small as -5.89507143187e-12. Allowing negative dual variable(s) as small as -1.10735114654e-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 -2.78073484378e-12. Allowing negative dual variable(s) as small as -7.11385963158e-12. Allowing negative dual variable(s) as small as -1.34974632382e-11. Allowing negative dual variable(s) as small as -1.37365405509e-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 -3.42411527421e-11. Allowing negative dual variable(s) as small as -3.57318940086e-11. Allowing negative dual variable(s) as small as -3.97097853545e-13. Allowing negative dual variable(s) as small as -5.67084368114e-11. Solving took 4 GP solves and 2.32 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 -4.11348472645e-13. Allowing negative dual variable(s) as small as -1.80527272818e-11. Allowing negative dual variable(s) as small as -7.28761708098e-11. Allowing negative dual variable(s) as small as -1.43013595758e-11. Solving took 4 GP solves and 1.72 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -7.71939456801e-12. Allowing negative dual variable(s) as small as -3.41417311089e-11. Allowing negative dual variable(s) as small as -2.09263509299e-11. Allowing negative dual variable(s) as small as -2.11382092385e-11. Allowing negative dual variable(s) as small as -2.13859069342e-11. Allowing negative dual variable(s) as small as -4.89425297165e-12. Allowing negative dual variable(s) as small as -1.04703748926e-11. Allowing negative dual variable(s) as small as -5.89810806532e-12. Allowing negative dual variable(s) as small as -1.10749979066e-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 -2.75601785317e-12. Allowing negative dual variable(s) as small as -7.11391893744e-12. Allowing negative dual variable(s) as small as -1.34973961261e-11. Allowing negative dual variable(s) as small as -1.37367534882e-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 -3.42486666858e-11. Allowing negative dual variable(s) as small as -3.57352937202e-11. Allowing negative dual variable(s) as small as -3.97201170812e-13. Allowing negative dual variable(s) as small as -5.67085168812e-11. Solving took 4 GP solves and 2.14 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 -4.04356235995e-13. Allowing negative dual variable(s) as small as -1.80514696073e-11. Allowing negative dual variable(s) as small as -7.28752973765e-11. Allowing negative dual variable(s) as small as -1.43021757631e-11. Solving took 4 GP solves and 1.4 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531