Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180605124826)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.246974729700149e-14.
Allowing negative dual variable(s) as small as -7.728409925911173e-14.
Allowing negative dual variable(s) as small as -1.510783685654271e-13.
Allowing negative dual variable(s) as small as -1.4831625511080304e-13.
Solving took 4 GP solves and 2.95 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.0791836014862923e-14.
Allowing negative dual variable(s) as small as -7.418718417362413e-14.
Allowing negative dual variable(s) as small as -1.5274240205975786e-13.
Allowing negative dual variable(s) as small as -1.497257179350342e-13.
Solving took 4 GP solves and 3.2 seconds.
Allowing negative dual variable(s) as small as -5.185851748024106e-13.
Allowing negative dual variable(s) as small as -1.4298198042217436e-12.
Allowing negative dual variable(s) as small as -4.431108258096117e-13.
Allowing negative dual variable(s) as small as -4.44583606040716e-13.
Allowing negative dual variable(s) as small as -1.2975900735845425e-12.
Allowing negative dual variable(s) as small as -1.089698210138268e-12.
Allowing negative dual variable(s) as small as -1.0900960039153529e-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 -2.892651396191326e-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 -2.5134842759571663e-14.
Allowing negative dual variable(s) as small as -5.69583973841754e-12.
Allowing negative dual variable(s) as small as -2.0879079591247533e-11.
Allowing negative dual variable(s) as small as -2.088081512758397e-11.
Solving took 4 GP solves and 2.69 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.99 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.191680418903388e-13.
Allowing negative dual variable(s) as small as -1.430319404582825e-12.
Allowing negative dual variable(s) as small as -4.43910533332037e-13.
Allowing negative dual variable(s) as small as -4.4508147167832135e-13.
Allowing negative dual variable(s) as small as -1.2959123791428384e-12.
Allowing negative dual variable(s) as small as -1.0908242625146114e-12.
Allowing negative dual variable(s) as small as -1.0918740954782291e-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 -4.844215306665234e-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 -2.5469076984239644e-14.
Allowing negative dual variable(s) as small as -5.695920021020844e-12.
Allowing negative dual variable(s) as small as -2.087900719539447e-11.
Allowing negative dual variable(s) as small as -2.0880802974434653e-11.
Solving took 4 GP solves and 2.9 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.87 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error