Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180420143542)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.866060233729932e-14.
Allowing negative dual variable(s) as small as -8.0181087463993e-14.
Allowing negative dual variable(s) as small as -1.5479327888923144e-13.
Allowing negative dual variable(s) as small as -1.4839822079504295e-13.
Solving took 4 GP solves and 1.55 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.964505790991616e-14.
Allowing negative dual variable(s) as small as -8.121021216611624e-14.
Allowing negative dual variable(s) as small as -1.5003319767115109e-13.
Allowing negative dual variable(s) as small as -1.475794313143819e-13.
Solving took 4 GP solves and 1.45 seconds.
Allowing negative dual variable(s) as small as -5.233175004448753e-13.
Allowing negative dual variable(s) as small as -5.131260000235116e-13.
Allowing negative dual variable(s) as small as -5.149561332906671e-13.
Allowing negative dual variable(s) as small as -5.143264286688876e-13.
Allowing negative dual variable(s) as small as -2.3353151010208073e-13.
Allowing negative dual variable(s) as small as -1.8217307003187688e-14.
Allowing negative dual variable(s) as small as -1.2586088855154332e-12.
Allowing negative dual variable(s) as small as -1.2600681132193814e-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 -1.5040052536718918e-14.
Allowing negative dual variable(s) as small as -1.1440935004936037e-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 -5.4341307084675844e-11.
Allowing negative dual variable(s) as small as -6.44971737162627e-12.
Allowing negative dual variable(s) as small as -1.9339134504895212e-11.
Allowing negative dual variable(s) as small as -1.935448289073903e-11.
Solving took 4 GP solves and 1.56 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.07 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.218204340851074e-13.
Allowing negative dual variable(s) as small as -5.102862576933376e-13.
Allowing negative dual variable(s) as small as -5.147601095378818e-13.
Allowing negative dual variable(s) as small as -5.157575755365684e-13.
Allowing negative dual variable(s) as small as -2.379684990727604e-13.
Allowing negative dual variable(s) as small as -1.8514595238883214e-14.
Allowing negative dual variable(s) as small as -1.2583791430750835e-12.
Allowing negative dual variable(s) as small as -1.2580448835453062e-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 -1.9734214262712158e-14.
Allowing negative dual variable(s) as small as -1.1469774782724151e-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 -5.434125387268967e-11.
Allowing negative dual variable(s) as small as -6.449645742311555e-12.
Allowing negative dual variable(s) as small as -1.9339201752084974e-11.
Allowing negative dual variable(s) as small as -1.9354510372537716e-11.
Solving took 4 GP solves and 1.33 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.09 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error