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!
Metadata
Metadata
Assignees
Labels
Type
Projects
Status
Backlog