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AerodynamicsAny problem to be worked on top of RocketPy's AerodynamicAny problem to be worked on top of RocketPy's AerodynamicEnhancementNew feature or request, including adjustments in current codesNew feature or request, including adjustments in current codes
Description
I noticed that RocketPy currently doesn’t account for Coriolis effects in its equations.
I made a few local modifications to include this behavior and found that, for a rocket with a 3 km apogee, the deviation at the impact point is less than 10 meters.
Since these changes were minimal, I thought you might be interested in checking them out.
Let me know if you're interested!
Gui-FernandesBR
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AerodynamicsAny problem to be worked on top of RocketPy's AerodynamicAny problem to be worked on top of RocketPy's AerodynamicEnhancementNew feature or request, including adjustments in current codesNew feature or request, including adjustments in current codes