Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171031154003)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.82675054839e-12.
Allowing negative dual variable(s) as small as -9.65608539308e-12.
Allowing negative dual variable(s) as small as -3.17928842974e-13.
Allowing negative dual variable(s) as small as -3.65498863814e-13.
Solving took 4 GP solves and 6.3 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.08564240268e-12.
Allowing negative dual variable(s) as small as -1.84754355911e-11.
Allowing negative dual variable(s) as small as -3.7652129678e-13.
Allowing negative dual variable(s) as small as -4.87296834828e-13.
Solving took 4 GP solves and 5.15 seconds.
Allowing negative dual variable(s) as small as -2.31563171416e-11.
Allowing negative dual variable(s) as small as -8.79606110171e-12.
Allowing negative dual variable(s) as small as -1.9882921698e-11.
Allowing negative dual variable(s) as small as -7.658047807e-12.
Allowing negative dual variable(s) as small as -7.69007774126e-12.
Allowing negative dual variable(s) as small as -2.36077069352e-11.
Allowing negative dual variable(s) as small as -1.17878174669e-11.
Allowing negative dual variable(s) as small as -1.19823040379e-11.
Allowing negative dual variable(s) as small as -1.17695687181e-11.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.73231923198e-11.
Allowing negative dual variable(s) as small as -1.24209510949e-11.
Allowing negative dual variable(s) as small as -7.11343690115e-12.
Allowing negative dual variable(s) as small as -6.647370588e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.45672978092e-12.
Allowing negative dual variable(s) as small as -2.39999687701e-12.
Allowing negative dual variable(s) as small as -7.67871605661e-11.
Allowing negative dual variable(s) as small as -8.54775459241e-11.
Solving took 4 GP solves and 2.69 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.93065050994e-12.
Allowing negative dual variable(s) as small as -3.89223926527e-11.
Allowing negative dual variable(s) as small as -5.40927454738e-11.
Allowing negative dual variable(s) as small as -5.45062701571e-11.
Solving took 4 GP solves and 5.64 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.31171540244e-11.
Allowing negative dual variable(s) as small as -8.77722200476e-12.
Allowing negative dual variable(s) as small as -1.98526334261e-11.
Allowing negative dual variable(s) as small as -7.6976619523e-12.
Allowing negative dual variable(s) as small as -7.7017558997e-12.
Allowing negative dual variable(s) as small as -2.36118769936e-11.
Allowing negative dual variable(s) as small as -1.17900551518e-11.
Allowing negative dual variable(s) as small as -1.19775087201e-11.
Allowing negative dual variable(s) as small as -1.17694687546e-11.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.73250484739e-11.
Allowing negative dual variable(s) as small as -1.24191598845e-11.
Allowing negative dual variable(s) as small as -7.11369060446e-12.
Allowing negative dual variable(s) as small as -6.64710485005e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.45701566809e-12.
Allowing negative dual variable(s) as small as -2.40005142339e-12.
Allowing negative dual variable(s) as small as -7.67770144114e-11.
Allowing negative dual variable(s) as small as -8.54888592358e-11.
Solving took 4 GP solves and 2.19 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.93414207461e-12.
Allowing negative dual variable(s) as small as -3.89348275842e-11.
Allowing negative dual variable(s) as small as -5.41039006131e-11.
Allowing negative dual variable(s) as small as -5.45107899791e-11.
Solving took 4 GP solves and 1.49 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error