Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171112203837)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.44635171895e-13.
Allowing negative dual variable(s) as small as -1.21743760906e-13.
Allowing negative dual variable(s) as small as -3.00603509099e-12.
Allowing negative dual variable(s) as small as -4.71575903327e-13.
Solving took 4 GP solves and 12.3 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.85108742171e-13.
Allowing negative dual variable(s) as small as -1.62160345915e-12.
Allowing negative dual variable(s) as small as -2.48449177898e-12.
Allowing negative dual variable(s) as small as -2.9895339676e-12.
Solving took 4 GP solves and 59 seconds.
Allowing negative dual variable(s) as small as -3.59982009479e-12.
Allowing negative dual variable(s) as small as -1.58838827508e-12.
Allowing negative dual variable(s) as small as -1.77693363496e-12.
Allowing negative dual variable(s) as small as -7.77845669819e-13.
Allowing negative dual variable(s) as small as -7.78236849963e-13.
Allowing negative dual variable(s) as small as -2.84198012346e-13.
Allowing negative dual variable(s) as small as -1.09922964828e-12.
Allowing negative dual variable(s) as small as -1.06908416581e-12.
Allowing negative dual variable(s) as small as -1.06245437795e-12.
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 -2.27321351846e-12.
Allowing negative dual variable(s) as small as -7.24680732089e-14.
Allowing negative dual variable(s) as small as -1.20500614695e-13.
Allowing negative dual variable(s) as small as -1.21676323531e-13.
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 -2.64163285987e-12.
Allowing negative dual variable(s) as small as -1.97771309313e-12.
Allowing negative dual variable(s) as small as -1.99756477207e-12.
Solving took 4 GP solves and 44.6 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.8492672591e-12.
Solving took 4 GP solves and 1.14 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.60244820086e-12.
Allowing negative dual variable(s) as small as -1.58806214706e-12.
Allowing negative dual variable(s) as small as -1.7783404957e-12.
Allowing negative dual variable(s) as small as -7.78516140443e-13.
Allowing negative dual variable(s) as small as -7.78319249328e-13.
Allowing negative dual variable(s) as small as -2.82164916432e-13.
Allowing negative dual variable(s) as small as -1.09887088578e-12.
Allowing negative dual variable(s) as small as -1.06861134525e-12.
Allowing negative dual variable(s) as small as -1.0627882038e-12.
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 -2.26801997322e-12.
Allowing negative dual variable(s) as small as -7.11788484056e-14.
Allowing negative dual variable(s) as small as -1.21016803349e-13.
Allowing negative dual variable(s) as small as -1.21138017152e-13.
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 -2.64364782769e-12.
Allowing negative dual variable(s) as small as -1.97688730351e-12.
Allowing negative dual variable(s) as small as -1.99449322314e-12.
Solving took 4 GP solves and 14.9 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.8526586435e-12.
Solving took 4 GP solves and 1.56 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error