![20 points] The following nonlinear differential equations describe the motion of a body in orbit around two much heavier bodi](https://media.cheggcdn.com/media%2F14d%2F14de9203-0f7c-4ae5-a41a-ddd8939d3690%2FphpMJXbZn.png)
matlab is being very difficult for me in this question
20 points] The following nonlinear differential equations describe the motion of a body in orbit around two much heavier bodies. An example would be an Apollo capsule in an Earth-moon orbit. The three bodies determine a two-dimensional Cartesian plane in space The origin is at the center of mass of the two heavy bodies, the x-axis is the line through these two bodies, and the distance between their
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