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## Main Question or Discussion Point

This is similar to finding the net force of a moon around and planet and the planet around the sun but in perfect circular orbits in 2d without consideration for gravitational effects.

Does anyone have a solution? If not theres a complicated paper that could be simplified from nasa in the 1930s out there. Or some parabolic equations with conic sections and calculus and vectors could be used.

The exact details for this is that a shaft has a fixed center on one end and the other end is a center of rotation for another shaft which rotates at the same speed but relative to the inner shaft. So at theta=0, they are both pointing the same direction with maximum radius. At theta=pi the farther rotation will be pointing to the center and will have the shortest radius. The mass is at the end of the outer shaft, assuming no weight for the shafts.

I'm not sure, but I think there are 2 sources for acceleration to find force. One is the normal force from rotation and the other is the relative acceleration caused by the outer shaft.

Any help would be appreciated, thanks.

Does anyone have a solution? If not theres a complicated paper that could be simplified from nasa in the 1930s out there. Or some parabolic equations with conic sections and calculus and vectors could be used.

The exact details for this is that a shaft has a fixed center on one end and the other end is a center of rotation for another shaft which rotates at the same speed but relative to the inner shaft. So at theta=0, they are both pointing the same direction with maximum radius. At theta=pi the farther rotation will be pointing to the center and will have the shortest radius. The mass is at the end of the outer shaft, assuming no weight for the shafts.

I'm not sure, but I think there are 2 sources for acceleration to find force. One is the normal force from rotation and the other is the relative acceleration caused by the outer shaft.

Any help would be appreciated, thanks.