Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20190422173205)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.2147088730469804e-14.
Allowing negative dual variable(s) as small as -7.406401880682978e-14.
Allowing negative dual variable(s) as small as -1.51386715663282e-13.
Allowing negative dual variable(s) as small as -1.4989311875046596e-13.
Solving took 4 GP solves and 2.35 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.341603895314684e-14.
Allowing negative dual variable(s) as small as -7.225470222138597e-14.
Allowing negative dual variable(s) as small as -1.5246658102707755e-13.
Allowing negative dual variable(s) as small as -1.4918968838095736e-13.
Solving took 4 GP solves and 1.79 seconds.
Allowing negative dual variable(s) as small as -5.191281432503914e-13.
Allowing negative dual variable(s) as small as -1.4286974381327866e-12.
Allowing negative dual variable(s) as small as -4.446356477449953e-13.
Allowing negative dual variable(s) as small as -4.4502942997404205e-13.
Allowing negative dual variable(s) as small as -1.2955235842437851e-12.
Allowing negative dual variable(s) as small as -1.0910772068814523e-12.
Allowing negative dual variable(s) as small as -1.0910409945288913e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -6.518223460982853e-16.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.496723526810077e-14.
Allowing negative dual variable(s) as small as -5.695955076485218e-12.
Allowing negative dual variable(s) as small as -2.0879074706884982e-11.
Allowing negative dual variable(s) as small as -2.0880834856966546e-11.
Solving took 4 GP solves and 2.47 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.15 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.174281142439341e-13.
Allowing negative dual variable(s) as small as -1.4293635719475617e-12.
Allowing negative dual variable(s) as small as -4.4556199008116693e-13.
Allowing negative dual variable(s) as small as -4.4543188582046866e-13.
Allowing negative dual variable(s) as small as -1.2959843701670914e-12.
Allowing negative dual variable(s) as small as -1.0911278391229073e-12.
Allowing negative dual variable(s) as small as -1.0909643414352965e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.506822573585248e-14.
Allowing negative dual variable(s) as small as -5.695966841614037e-12.
Allowing negative dual variable(s) as small as -2.087899999299391e-11.
Allowing negative dual variable(s) as small as -2.0880913262703658e-11.
Solving took 4 GP solves and 1.69 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.29 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error

/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped.
  warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning)