Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171031154037)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.78414398112e-14.
Allowing negative dual variable(s) as small as -1.03700468351e-13.
Allowing negative dual variable(s) as small as -3.16587034366e-17.
Allowing negative dual variable(s) as small as -4.24139889876e-16.
Solving took 4 GP solves and 8.16 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.0313581586e-13.
Allowing negative dual variable(s) as small as -1.00300410338e-13.
Allowing negative dual variable(s) as small as -3.09214459593e-16.
Solving took 4 GP solves and 9.71 seconds.
Allowing negative dual variable(s) as small as -3.86090898835e-12.
Allowing negative dual variable(s) as small as -1.66069328428e-12.
Allowing negative dual variable(s) as small as -7.36417871128e-13.
Allowing negative dual variable(s) as small as -7.4329604971e-13.
Allowing negative dual variable(s) as small as -7.43858100116e-13.
Allowing negative dual variable(s) as small as -2.27451304319e-13.
Allowing negative dual variable(s) as small as -9.97220210054e-13.
Allowing negative dual variable(s) as small as -1.01334750053e-12.
Allowing negative dual variable(s) as small as -1.01675157009e-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 -1.47270867376e-13.
Allowing negative dual variable(s) as small as -4.35483897207e-14.
Allowing negative dual variable(s) as small as -2.80755236767e-14.
Allowing negative dual variable(s) as small as -2.79579961612e-14.
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 -6.23755074217e-13.
Allowing negative dual variable(s) as small as -3.94711316723e-14.
Allowing negative dual variable(s) as small as -1.06914560122e-13.
Allowing negative dual variable(s) as small as -1.07973145053e-13.
Solving took 4 GP solves and 14.6 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 5.02 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.85932258373e-12.
Allowing negative dual variable(s) as small as -1.66041486116e-12.
Allowing negative dual variable(s) as small as -7.36598282369e-13.
Allowing negative dual variable(s) as small as -7.44238004557e-13.
Allowing negative dual variable(s) as small as -7.43511155421e-13.
Allowing negative dual variable(s) as small as -2.33744664249e-13.
Allowing negative dual variable(s) as small as -9.97764262704e-13.
Allowing negative dual variable(s) as small as -1.01490864324e-12.
Allowing negative dual variable(s) as small as -1.01623169515e-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 -1.38447413256e-13.
Allowing negative dual variable(s) as small as -4.36846739338e-14.
Allowing negative dual variable(s) as small as -2.77274947794e-14.
Allowing negative dual variable(s) as small as -2.89028783546e-14.
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 -6.23101668342e-13.
Allowing negative dual variable(s) as small as -4.02834556446e-14.
Allowing negative dual variable(s) as small as -1.07358724823e-13.
Allowing negative dual variable(s) as small as -1.0917069691e-13.
Solving took 4 GP solves and 25.5 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.6 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error