ComputeMeanElements method crashes sometimes
ComputeMeanElements method may crash when provided SpacecraftState
includes accelerations.
The bug occurs in AbstractGaussianContribution$IntegrableFunction.value
function. I cannot tell whether dt is not correctly computed
(normalisation problem ?) or the accelerations are not correctly taken
into account. Yet the problem probably lies in that part of the code.
Please find attached a file containing a test which reproduces the bug. The test is heavily based on testIssue339. The getLeoState method has been changed so that the initial state is propagated 30 minutes. This way the state provided to computeMeanState() includes accelerations.
(from redmine: issue id 345, created on 2017-06-19, closed on 2017-07-27)
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