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Fixed RAAN and added Petropoulos test cases #12

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Jan 8, 2017
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ChristopherRabotin
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Closes #8.

I should be able to keep the rest of the OEs free, but this is not
happening!
Had to update the signation to NewOptimalΔOrbit.
TestMultiCorrectOE leads to a panic. I suspect it's due to the
eccentricity correction, but I'm not sure yet. If not, it's due to the
Ruggerio factor.

Note: the inclination change does not work at all with the provided
equation, regardless of the duration of propagation (I tried a 20 times
longer propagation).
Also ensured that the angle conversaions always lead to positive angles.
WEIRD: norm(R) is different from GetRNorm() in the Vallado test case,
but it works perfectly fine (within some numerical approximation of
~4km) in the astrocro propagation.
Also tried to improve the test coverage, but kinda failed.
I don't know why the code in the spacecraft part for dropping the cargo
does not execute. That's a big question mark but not important right
now. First I gotta solve those damn orbital corrections.
But they all either fail or panic.
@ChristopherRabotin ChristopherRabotin merged commit d87a9f0 into master Jan 8, 2017
@ChristopherRabotin ChristopherRabotin deleted the issue-8 branch January 8, 2017 00:36
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