Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180124110710)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.8911911967012252e-13.
Allowing negative dual variable(s) as small as -9.018350302647526e-14.
Allowing negative dual variable(s) as small as -5.209895015401145e-14.
Allowing negative dual variable(s) as small as -5.5362398693192816e-14.
Solving took 4 GP solves and 31.7 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.9406004581057346e-13.
Allowing negative dual variable(s) as small as -9.225953334635051e-14.
Allowing negative dual variable(s) as small as -5.613261591652652e-14.
Allowing negative dual variable(s) as small as -5.809892497654623e-14.
Solving took 4 GP solves and 32.7 seconds.
Allowing negative dual variable(s) as small as -5.97389325507347e-13.
Allowing negative dual variable(s) as small as -1.4370050288592395e-12.
Allowing negative dual variable(s) as small as -1.6874999661520285e-12.
Allowing negative dual variable(s) as small as -1.6871053165612437e-12.
Allowing negative dual variable(s) as small as -1.3483561055877002e-12.
Allowing negative dual variable(s) as small as -2.2117535667526278e-12.
Allowing negative dual variable(s) as small as -2.2624567150297814e-13.
Allowing negative dual variable(s) as small as -2.297103479653728e-13.
MTOW [lbs] = 134.67
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 = 20.615
speed at top of climb [m/s] = 25.153
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.521
Allowing negative dual variable(s) as small as -1.7898310871594658e-12.
Allowing negative dual variable(s) as small as -2.0402798374397069e-13.
Allowing negative dual variable(s) as small as -2.2046080239146448e-13.
Allowing negative dual variable(s) as small as -2.257480227058073e-13.
optimum loiter speed for min power, start of loiter [m/s] = 23.910
optimum loiter speed for min power, end of loiter [m/s] = 16.760
optimum cruise speed, inbound [m/s] = 31.821
optimum cruise speed, outbound [m/s] = 23.768
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.2877487374343875e-11.
Allowing negative dual variable(s) as small as -8.751189831495578e-12.
Allowing negative dual variable(s) as small as -8.175400359858772e-12.
Allowing negative dual variable(s) as small as -8.174520336218993e-12.
Solving took 4 GP solves and 52.5 seconds.
Max Speed [m/s]: 66.56
Beginning signomial solve.
Solving took 4 GP solves and 7.89 seconds.
Max payload weight [lbf] = 12.624
Max take off weight [lbf] = 145.409
Allowing negative dual variable(s) as small as -5.972227920536533e-13.
Allowing negative dual variable(s) as small as -1.4368818634924452e-12.
Allowing negative dual variable(s) as small as -1.687537262706762e-12.
Allowing negative dual variable(s) as small as -1.6869864880031393e-12.
Allowing negative dual variable(s) as small as -1.3518262030609574e-12.
Allowing negative dual variable(s) as small as -2.2113281258201445e-12.
Allowing negative dual variable(s) as small as -2.2699116891677917e-13.
Allowing negative dual variable(s) as small as -2.3078674388221643e-13.
MTOW [lbs] = 134.67
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 = 20.615
speed at top of climb [m/s] = 25.153
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.521
Allowing negative dual variable(s) as small as -1.7807786495405153e-12.
Allowing negative dual variable(s) as small as -2.0147533814907082e-13.
Allowing negative dual variable(s) as small as -2.271245257839949e-13.
Allowing negative dual variable(s) as small as -2.1910056234586417e-13.
optimum loiter speed for min power, start of loiter [m/s] = 23.910
optimum loiter speed for min power, end of loiter [m/s] = 16.760
optimum cruise speed, inbound [m/s] = 31.821
optimum cruise speed, outbound [m/s] = 23.768
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.2877488295783373e-11.
Allowing negative dual variable(s) as small as -8.751140761285448e-12.
Allowing negative dual variable(s) as small as -8.17525646000224e-12.
Allowing negative dual variable(s) as small as -8.174429209238154e-12.
Solving took 4 GP solves and 49 seconds.
Max Speed [m/s]: 66.56
Beginning signomial solve.
Solving took 4 GP solves and 8.78 seconds.
Max payload weight [lbf] = 12.624
Max take off weight [lbf] = 145.409
	

Standard Error