Published: 25 October, 2024 | Volume 7 - Issue 2 | Pages: 148-153
Figure 2:
Results of numerical simulations of motion of a model system: point mass in central force field from point source mass on an elliptical orbit. The starting position and velocity vectors are: r0 = (0.2,0) [a.u.] (apoapsis), v0 = (0,0.8 c) [a.u.]. We observe the orbit’s precession, for which the Fp component is responsible. The direction of precession is in the direction of the velocity vector.
Read Full Article HTML DOI: 10.29328/journal.ijpra.1001100 Cite this Article Read Full Article PDF
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