04:27
Restricted 3-Body Problem With Osculating Orbits
04:01
3-Body Lagrange Problem With Osculating Orbits
01:06
4-Body Lagrange Problem With Osculating Orbits
04:27
Pythagorean 3-Body Problem With Osculating Orbits
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About
Results of our work on celestial mechanics, or more specifically, the calculation of osculating orbits in n-body problems. The osculating orbit of an object in space is the gravitational Kepler orbit that it would have if perturbations were not present. For each body exactly one osculating orbit exists in any moment of time, represented by the thin lines in the animations.
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Michael & Volker Dörr
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