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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).
| Version: | 0.2.0 |
| Depends: | R (≥ 4.1.0) |
| Imports: | dplyr, ggplot2, Rcpp, tibble |
| LinkingTo: | Rcpp |
| Suggests: | plotly, gganimate, gifski, magick, knitr, rmarkdown, pkgdown, testthat (≥ 3.0.0) |
| Published: | 2026-04-21 |
| DOI: | 10.32614/CRAN.package.orbitr |
| Author: | Dave Rosenman [aut, cre] |
| Maintainer: | Dave Rosenman <dave.rosenman.data at gmail.com> |
| BugReports: | https://github.com/DRosenman/orbitr/issues |
| License: | MIT + file LICENSE |
| URL: | https://orbit-r.com/, https://github.com/DRosenman/orbitr |
| NeedsCompilation: | yes |
| Materials: | README, NEWS |
| CRAN checks: | orbitr results |
| Package source: | orbitr_0.2.0.tar.gz |
| Windows binaries: | r-release: orbitr_0.2.0.zip, r-oldrel: orbitr_0.2.0.zip |
| macOS binaries: | r-release (arm64): orbitr_0.2.0.tgz, r-oldrel (arm64): orbitr_0.2.0.tgz, r-release (x86_64): orbitr_0.2.0.tgz, r-oldrel (x86_64): orbitr_0.2.0.tgz |
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These binaries (installable software) and packages are in development.
They may not be fully stable and should be used with caution. We make no claims about them.
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