95 lines
4.0 KiB
Markdown
95 lines
4.0 KiB
Markdown
# astrokit
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A highly-performant astrodynamics engine, written in Rust. Force models, propagation, reference
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frames, spacecraft geometry and measurement models — built on
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[`ordinary-diffeq`](https://crates.io/crates/ordinary-diffeq) for integration,
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and generic over the scalar type so that any propagation you can solve you can
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also differentiate.
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## Status
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The crate is still being built to a milestone plan:
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- **M1** — the core subset: two-body and spherical-harmonic gravity, drag,
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third-body, cannonball SRP, GCRF/ITRF frames, ground stations and the four
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measurement types, with a validation suite against Orekit reference
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trajectories.
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- **M2** — general-purpose completion: higher-degree gravity fields, more
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density models, box-wing SRP and eclipses, maneuvers, covariance propagation,
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relative motion, TLE and CCSDS I/O.
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The tables under [Validation](#validation) and [Performance](#performance) are
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the acceptance criteria.
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## Conventions
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- Everything is SI
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- Time is typed, using `hifitime`
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- US English spelling
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## Foundations
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These are depended on, not reimplemented.
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| Crate | License | Provides |
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| [`hifitime`](https://crates.io/crates/hifitime) 4.3 | MPL-2.0 | TAI/TT/ET/TDB/UTC/GPS time scales, leap seconds |
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| [`anise`](https://crates.io/crates/anise) 0.10 | MPL-2.0 | Reference frames, planetary ephemerides, SPICE-format kernels |
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| [`ordinary-diffeq`](https://crates.io/crates/ordinary-diffeq) 0.4 | MIT | Adaptive integration, dense output, callbacks, autodiff |
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## Validation
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Before we can make a highly-performant propagator, we have to make a *correct* propagator.
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1. **Orekit reference fixtures.** A committed, rerunnable generation script
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produces reference trajectories and observations; the data lands under
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`tests/fixtures/` with the Orekit version, force-model configuration and
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generation date recorded beside it; Rust tests assert agreement within
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declared tolerances.
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2. **Analytic invariants.**: ie, "does a two-body orbit close back in on itself after one-period?" and similar conservation-tests, meant to run fast as unit tests to ensure that nothing has broken.
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3. **ANISE cross-checks.** Frame transformations and ephemeris lookups against
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ANISE's own validated values, confirming that we are calling it correctly.
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Every fixture comparison matches gravity degree and order, density model,
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third-body ephemeris source and integrator tolerances; anything that cannot be
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matched is documented and its contribution bounded.
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| Case | Target | Achieved | Test |
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| 1-day LEO arc, full matched force model | 1 m position, 1 mm/s velocity | not yet measured | — |
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| 6-day LEO arc | to be set from the 1-day result | not yet measured | — |
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| GEO arc, including a time-varying-area change | to be set | not yet measured | — |
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| Two-body energy and angular momentum | integrator tolerance | not yet measured | — |
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| Two-body closure over N periods | integrator tolerance | not yet measured | — |
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| J2 secular nodal regression and apsidal rotation | to be set | not yet measured | — |
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| RA/DEC, range, range-rate, az/el against Orekit | to be set | not yet measured | — |
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## Performance
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Measured against `nyx-space` and Orekit on the same benchmarks with matched force
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models, on the same hardware. Neither publishes usable figures, so the references
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are measured here rather than cited.
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| Benchmark | astrokit | nyx-space | Orekit |
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| Two-body throughput (state-steps/s) | not yet measured | — | — |
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| Full-force LEO, 1 day | not yet measured | — | — |
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| Ensemble of N states, scaling vs. cores | not yet measured | — | — |
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## Development
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Enable the pre-commit hook once per clone:
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```sh
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git config core.hooksPath .githooks
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```
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It runs `cargo fmt --check`, `cargo clippy --all-targets --all-features -- -D
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warnings`, and a US English spelling check. `git commit --no-verify` skips it.
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Tests and docs are left out to keep it under a few seconds; run `cargo test`
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yourself.
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## License
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MIT. See [LICENSE](./LICENSE).
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