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A lightweight, fully vectorized N-body physics engine built for the R ecosystem. Simulate and visualize complex orbital mechanics, celestial trajectories, and gravitational interactions using tidy data principles. Features multiple numerical integration methods, including the energy-conserving velocity Verlet algorithm (Verlet (1967) <doi:10.1103/PhysRev.159.98>), to ensure highly stable orbital propagation. Gravitational N-body methods follow Aarseth (2003, ISBN:0-521-43272-3).
Package details |
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| Author | Dave Rosenman [aut, cre] |
| Maintainer | Dave Rosenman <dave.rosenman.data@gmail.com> |
| License | MIT + file LICENSE |
| Version | 1.0.0 |
| URL | https://orbit-r.com/ https://github.com/DRosenman/orbitr |
| Package repository | View on CRAN |
| Installation |
Install the latest version of this package by entering the following in R:
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