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Passed

gpkit.tests.from_paths.TestFiles.test_gpkitmodels_GP_aircraft_tail_tail_tests_py_cvxopt (from gpkit.tests.from_paths.TestFiles-20180403161937)

Took 10 sec.

Standard Output

Using solver 'cvxopt'
Solving for 11 variables.
Solving took 0.0314 seconds.
Using solver 'cvxopt'
Solving for 5 variables.
Solving took 0.0227 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
Couldn't auto-differentiate linked variable cosminus1_GustL_(1,).
Couldn't auto-differentiate linked variable cosminus1_GustL_(3,).
Couldn't auto-differentiate linked variable cosminus1_GustL_(0,).
Couldn't auto-differentiate linked variable cosminus1_GustL_(4,).
Couldn't auto-differentiate linked variable cosminus1_GustL_(2,).
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1888111.4290 but bound is 700000.0000
Couldn't auto-differentiate linked variable cosminus1_GustL.1_(1,).
Couldn't auto-differentiate linked variable cosminus1_GustL.1_(2,).
Couldn't auto-differentiate linked variable cosminus1_GustL.1_(3,).
Couldn't auto-differentiate linked variable cosminus1_GustL.1_(4,).
Couldn't auto-differentiate linked variable cosminus1_GustL.1_(0,).
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1661196.4500 but bound is 700000.0000
	

Standard Error