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Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180605125229)

Took 29 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.191946690965345e-14.
Allowing negative dual variable(s) as small as -7.661579703999166e-14.
Allowing negative dual variable(s) as small as -1.3237382110592444e-13.
Allowing negative dual variable(s) as small as -1.2931669624016706e-13.
Solving took 4 GP solves and 4.57 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.556726511898093e-14.
Allowing negative dual variable(s) as small as -7.596635993867284e-14.
Allowing negative dual variable(s) as small as -1.3254577557048064e-13.
Allowing negative dual variable(s) as small as -1.2733347362625658e-13.
Solving took 4 GP solves and 4.65 seconds.
Allowing negative dual variable(s) as small as -7.634474649687029e-14.
Allowing negative dual variable(s) as small as -3.4044165056479336e-13.
Allowing negative dual variable(s) as small as -1.0203352919513353e-12.
Allowing negative dual variable(s) as small as -1.0212442870527472e-12.
Allowing negative dual variable(s) as small as -2.7782751143082263e-13.
Allowing negative dual variable(s) as small as -1.1539543463574137e-12.
Allowing negative dual variable(s) as small as -1.116056411783889e-12.
Allowing negative dual variable(s) as small as -1.1150540939804804e-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 -1.2095671686473963e-12.
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 -6.145424614951699e-11.
Allowing negative dual variable(s) as small as -1.454614044511487e-12.
Allowing negative dual variable(s) as small as -6.463225724134785e-12.
Allowing negative dual variable(s) as small as -6.468935310082912e-12.
Solving took 4 GP solves and 4.38 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.78 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -7.781318991928465e-14.
Allowing negative dual variable(s) as small as -3.391592562351775e-13.
Allowing negative dual variable(s) as small as -1.0211449741337475e-12.
Allowing negative dual variable(s) as small as -1.0225141046371622e-12.
Allowing negative dual variable(s) as small as -2.783667935914169e-13.
Allowing negative dual variable(s) as small as -1.153348602603646e-12.
Allowing negative dual variable(s) as small as -1.115789996205055e-12.
Allowing negative dual variable(s) as small as -1.11509174290092e-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 -1.2098022236783912e-12.
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 -6.145430782325643e-11.
Allowing negative dual variable(s) as small as -1.454631685957847e-12.
Allowing negative dual variable(s) as small as -6.463367573777846e-12.
Allowing negative dual variable(s) as small as -6.468765131317051e-12.
Solving took 4 GP solves and 3.36 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 4.17 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error