Drag Force not properly inplemented
I'm trying to implement OreKit in Matlab, and I've noticed I get identical orbit propagations with the drag force both on and off. SRP implements correctly, but drag force is not. I have tried multiple satellite classes (solar array box model and spherical) and multiple atmosphere models (exponential and Harris-Priester).
Attached is the .m file I'm using to implement OreKit.
(from redmine: issue id 191, created on 2015-03-05, closed on 2016-02-10)
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