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Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180418162455)

Took 2 min 34 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.910772731323235e-14.
Allowing negative dual variable(s) as small as -8.086023170483791e-14.
Allowing negative dual variable(s) as small as -1.489403218812857e-13.
Allowing negative dual variable(s) as small as -1.4871914463809865e-13.
Solving took 4 GP solves and 5.11 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.083377717182927e-14.
Allowing negative dual variable(s) as small as -8.24618151540335e-14.
Allowing negative dual variable(s) as small as -1.5020797106135575e-13.
Allowing negative dual variable(s) as small as -1.5280355106228605e-13.
Solving took 4 GP solves and 4.08 seconds.
Allowing negative dual variable(s) as small as -5.254859047898464e-13.
Allowing negative dual variable(s) as small as -5.12126799301349e-13.
Allowing negative dual variable(s) as small as -5.144860232286774e-13.
Allowing negative dual variable(s) as small as -5.159119659259304e-13.
Allowing negative dual variable(s) as small as -2.371683578694661e-13.
Allowing negative dual variable(s) as small as -1.8748457647488337e-14.
Allowing negative dual variable(s) as small as -1.25984986332206e-12.
Allowing negative dual variable(s) as small as -1.2573585835701229e-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 -1.865087945196464e-14.
Allowing negative dual variable(s) as small as -1.147959765440687e-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 -5.434118232815766e-11.
Allowing negative dual variable(s) as small as -6.449626444836374e-12.
Allowing negative dual variable(s) as small as -1.9339135199224e-11.
Allowing negative dual variable(s) as small as -1.9354639365597066e-11.
Solving took 4 GP solves and 62.9 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 24.4 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.231353544798978e-13.
Allowing negative dual variable(s) as small as -5.120140422754105e-13.
Allowing negative dual variable(s) as small as -5.157332894079047e-13.
Allowing negative dual variable(s) as small as -5.13394882162288e-13.
Allowing negative dual variable(s) as small as -2.3714450542167143e-13.
Allowing negative dual variable(s) as small as -1.8200935550383157e-14.
Allowing negative dual variable(s) as small as -1.2596450575316775e-12.
Allowing negative dual variable(s) as small as -1.25889587383049e-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 -2.023598302813845e-14.
Allowing negative dual variable(s) as small as -1.145422732357071e-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 -5.434120947524598e-11.
Allowing negative dual variable(s) as small as -6.4497070699850955e-12.
Allowing negative dual variable(s) as small as -1.9339230352417136e-11.
Allowing negative dual variable(s) as small as -1.9354665893742532e-11.
Solving took 4 GP solves and 12.2 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 31.1 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error