Passed

gpkit.tests.from_paths.TestFiles.test_gpkitmodels_GP_aircraft_fuselage_test_fuselage_py_cvxopt (from gpkit.tests.from_paths.TestFiles-20180423140223)

Standard Output

Using solver 'cvxopt'
Solving for 11 variables.
Solving took 0.00795 seconds.
Using solver 'cvxopt'
Solving for 8 variables.
Solving took 0.00874 seconds.
Using solver 'cvxopt'
Solving for 24 variables.
Solving took 0.0285 seconds.
Using solver 'cvxopt'
Solving for 24 variables.
Solving took 0.027 seconds.
Using solver 'cvxopt'
Solving for 13 variables.
Solving took 0.0117 seconds.
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220952.3405 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.5667 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223840.1738 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223840.1106 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1849726.5742 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1849726.5540 but bound is 1000000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 2197590.3832 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1681137.7135 but bound is 700000.0000
	

Standard Error