Skip to content

Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180424140732)

Took 8.3 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.597503355605273e-14.
Allowing negative dual variable(s) as small as -7.888058695809663e-14.
Allowing negative dual variable(s) as small as -1.2774785569658054e-13.
Allowing negative dual variable(s) as small as -1.3102539886400422e-13.
Solving took 4 GP solves and 3.48 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.659183617197973e-14.
Allowing negative dual variable(s) as small as -7.817802395032603e-14.
Allowing negative dual variable(s) as small as -1.2992168105241397e-13.
Allowing negative dual variable(s) as small as -1.2793726581611375e-13.
Solving took 4 GP solves and 3.88 seconds.
Allowing negative dual variable(s) as small as -5.835371248708032e-13.
Allowing negative dual variable(s) as small as -3.3769948643014303e-13.
Allowing negative dual variable(s) as small as -1.0223163461609008e-12.
Allowing negative dual variable(s) as small as -1.021633732473104e-12.
Allowing negative dual variable(s) as small as -2.784875737134318e-13.
Allowing negative dual variable(s) as small as -1.1544811872980787e-12.
Allowing negative dual variable(s) as small as -1.1178500074378317e-12.
Allowing negative dual variable(s) as small as -1.1167763491314736e-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 -1.209899639243589e-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 -6.14543137619103e-11.
Allowing negative dual variable(s) as small as -1.4546096951958261e-12.
Allowing negative dual variable(s) as small as -6.463107858759021e-12.
Allowing negative dual variable(s) as small as -6.4689188643162015e-12.
Solving took 4 GP solves and 5.33 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.47 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.859587988432668e-13.
Allowing negative dual variable(s) as small as -3.391761697890683e-13.
Allowing negative dual variable(s) as small as -1.0238086420311099e-12.
Allowing negative dual variable(s) as small as -1.0214910514672049e-12.
Allowing negative dual variable(s) as small as -2.796316238458385e-13.
Allowing negative dual variable(s) as small as -1.1545995821753141e-12.
Allowing negative dual variable(s) as small as -1.1157918122436938e-12.
Allowing negative dual variable(s) as small as -1.116017434715788e-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 -1.2095468940667709e-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 -6.145434885750286e-11.
Allowing negative dual variable(s) as small as -1.4547132768300077e-12.
Allowing negative dual variable(s) as small as -6.463278355281351e-12.
Allowing negative dual variable(s) as small as -6.468909137161889e-12.
Solving took 4 GP solves and 2.98 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.87 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error