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llnl/SSAPy

SSAPy - Space Situational Awareness for Python

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SSAPy is a fast, flexible, high-fidelity orbital modeling and analysis tool for orbits spanning from low-Earth orbit into the cislunar regime.

For higher-level utilities, convenience workflows, plotting tools, GCRF-to-ITRF coordinate conversion helpers, Lambertian magnitude / brightness calculations, and related extensions, see the companion project SSAPy-Toolkit.

SSAPy includes:

  • Ability to define satellite parameters (area, mass, radiation and drag coefficients, etc.)
  • Support for multiple orbit representations and input types, including TLE-based initialization and Keplerian, equinoctial, and Kozai mean Keplerian elements
  • Fully customizable analytic force propagation models, including:
    • Earth gravity models (WGS84, EGM84, EGM96, EGM2008)
    • Lunar gravity models (point source and harmonic)
    • Radiation pressure (Earth and solar)
    • Forces for planets out to Neptune
    • Atmospheric drag models
    • Maneuvering with user-defined burn profiles
  • Multiple integrators, including SGP4, Runge-Kutta (4, 8, and 7/8), SciPy, Keplerian, and Taylor series methods
  • User-definable timesteps and orbit information retrieval times, allowing queries for quantities of interest such as magnitude, state vectors, TLEs, Keplerian elements, periapsis, apoapsis, specific angular momentum, and more
  • Ground- and space-based observer models
  • Lighting and visibility condition analysis
  • Multiple-hypothesis tracking (MHT) UCT linker
  • Vectorized computations using array broadcasting for efficient execution and easy deployment on HPC systems
  • Short-arc probabilistic orbit determination methods
  • Conjunction probability estimation
  • Built-in uncertainty quantification
  • Support for Monte Carlo runs and data fusion
  • Support for multiple coordinate frames and coordinate transformations, including GCRF, IERS, GCRS Cartesian, TEME Cartesian, RA/Dec, NTW, zenith/azimuth, apparent positions, and orthogonal tangent plane coordinates

Installation

For installation details, see the Installing SSAPy section of the documentation.

If you are looking for higher-level utilities or plotting-oriented workflows, you may also want to install or explore SSAPy-Toolkit.

Strict dependencies

The following Python packages are installed automatically when you install SSAPy:

Documentation

The documentation is hosted at:

https://LLNL.github.io/SSAPy/

The API documentation may also be explored interactively:

python3
import ssapy
help(ssapy)

Contributing

Contributing to SSAPy is straightforward. Please open a pull request targeting the main branch of the SSAPy repository.

For work that primarily concerns plotting, dashboards, convenience utilities, or higher-level workflows, please also consider whether the contribution belongs in the companion repository SSAPy-Toolkit.

Your PR must pass SSAPy's required CI checks. For local testing guidance, documentation builds, and Git workflow tips, see the Contribution Guide.

SSAPy's main branch contains the latest development work.

Releases

For stable installations, we recommend using one of SSAPy's tagged releases.

The latest release is always available from the releases/latest tag.

Code of Conduct

Please note that SSAPy has a Code of Conduct. By participating in the SSAPy community, you agree to abide by its rules.

Authors

SSAPy was developed with support from Lawrence Livermore National Laboratory's (LLNL) Laboratory Directed Research and Development (LDRD) Program under projects 19-SI-004 and 22-ERD-054, by the following individuals (in alphabetical order):

Many thanks go to SSAPy's other contributors.

Citing SSAPy

On GitHub, you can copy a citation in APA or BibTeX format via the "Cite this repository" button. If you prefer MLA or Chicago style citations, see the comments in CITATION.cff.

You may also cite the following publications (click here for BibTeX entries):

  • Yeager, T., Pruett, K., & Schneider, M. (2022). Unaided Dynamical Orbit Stability in the Cislunar Regime. Poster presentation, Cislunar Security Conference, USA.
  • Yeager, T., Pruett, K., & Schneider, M. (2023). Long-term N-body Stability in Cislunar Space. Poster presentation, Advanced Maui Optical and Space Surveillance (AMOS) Technologies Conference, USA.
  • Yeager, T., Pruett, K., & Schneider, M. (2023, September). Long-term N-body Stability in Cislunar Space. In S. Ryan (Ed.), Proceedings of the Advanced Maui Optical and Space Surveillance (AMOS) Technologies Conference (p. 208). Retrieved from https://amostech.com/TechnicalPapers/2023/Poster/Yeager.pdf

License

SSAPy is distributed under the terms of the MIT license. All new contributions must be made under the MIT license.

See the LICENSE and NOTICE files for details.

SPDX-License-Identifier: MIT

LLNL-CODE-862420

Documentation Inspiration

The structure and organization of this repository's documentation were inspired by the excellent design and layout of the Coffea project.

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A Python package allowing for fast and precise orbital modeling.

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