Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180417213750)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.092918696300799e-14.
Allowing negative dual variable(s) as small as -8.509816115664925e-14.
Allowing negative dual variable(s) as small as -1.5075917944584738e-13.
Allowing negative dual variable(s) as small as -1.5411023152056558e-13.
Solving took 4 GP solves and 6.8 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.824860551175483e-14.
Allowing negative dual variable(s) as small as -8.277189697536436e-14.
Allowing negative dual variable(s) as small as -1.509148708778163e-13.
Allowing negative dual variable(s) as small as -1.487152415102777e-13.
Solving took 4 GP solves and 8.92 seconds.
Allowing negative dual variable(s) as small as -5.238847550215198e-13.
Allowing negative dual variable(s) as small as -5.131919195155987e-13.
Allowing negative dual variable(s) as small as -5.145276565921009e-13.
Allowing negative dual variable(s) as small as -5.141945896847133e-13.
Allowing negative dual variable(s) as small as -2.381259252282053e-13.
Allowing negative dual variable(s) as small as -1.7711201429071455e-14.
Allowing negative dual variable(s) as small as -1.2604706774860253e-12.
Allowing negative dual variable(s) as small as -1.2588908865004966e-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 -2.1134569788694435e-14.
Allowing negative dual variable(s) as small as -1.1458217187565456e-13.
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 -5.4341287228423616e-11.
Allowing negative dual variable(s) as small as -6.44960076314152e-12.
Allowing negative dual variable(s) as small as -1.933919360383978e-11.
Allowing negative dual variable(s) as small as -1.9354601390330714e-11.
Solving took 4 GP solves and 3.95 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.75 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.224830984529305e-13.
Allowing negative dual variable(s) as small as -5.104579953174593e-13.
Allowing negative dual variable(s) as small as -5.146404136180394e-13.
Allowing negative dual variable(s) as small as -5.15042869464466e-13.
Allowing negative dual variable(s) as small as -2.383150100870868e-13.
Allowing negative dual variable(s) as small as -1.8240617349896127e-14.
Allowing negative dual variable(s) as small as -1.25937346488747e-12.
Allowing negative dual variable(s) as small as -1.2588659498505295e-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 -1.8063241874477498e-14.
Allowing negative dual variable(s) as small as -1.1316230071056754e-13.
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 -5.43412260154701e-11.
Allowing negative dual variable(s) as small as -6.44966438000101e-12.
Allowing negative dual variable(s) as small as -1.9339264300280052e-11.
Allowing negative dual variable(s) as small as -1.9354620194462143e-11.
Solving took 4 GP solves and 20.7 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.94 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error