nasabreakup

nasabreakup

Python Package IndexPython Package Index
Unavailable
This project is no longer available (or publicly accessible) from Python Package Index
Releases4
Frequency8 hours
Last Release
# NASA Breakup Model in Python
NASA Standard Breakup Model in Python is a Python library for simulating explosion and collision events in orbit using the NASA Standard Breakup Model. The breakup model was implemented based on the following works: NASA’s new breakup model of evolve 4.0 (Johnson et al.), and Proper Implementation of the 1998 NASA Breakup Model (Krisko et al.). ## Installation NASA Breakup Model in Python runs on Python 3.6 or higher (Python 3.8 is recommended): Currently the package is available using pip: ``` pip install nasabreakup ``` >*A conda distribution will be made available when the project is stable* ## Getting Started To use NASA Breakup Model in Python, you must first create a .yaml file to configure the simulation. This file has three required fields, the minimum characteristic length, the [simulation type](https://nasa-breakup-model-python.readthedocs.io/en/latest/_autosummary/nasabreakup.configuration.SimulationType.html), and the [satellite type](https://nasa-breakup-model-python.readthedocs.io/en/latest/_autosummary/nasabreakup.configuration.SatType.html) involved in the fragmentation event. Secondly, you must provide an implementation of [Satellite](https://nasa-breakup-model-python.readthedocs.io/en/latest/_autosummary/nasabreakup.satellite.Satellite.html). Once, you have those two criterion met you can perform the simulation as follows: ```python from nasabreakup.configuration import SimulationConfiguration from nasabreakup.model import FragmentationEvent config = SimulationConfiguration('data/simulation_config.yaml') event = FragmentationEvent(config, np.array([sat])) debris = event.run() ``` > An example configuration.yaml and Satellite implementation has been provided in `examples` ## Resulting Data Format | index | data | type | |-------|----------------------------|------------------------------------| | 0 | SatType (for internal use) | enum | | 1 | position | np.array (, 3), containing floats | | 2 | characteristic length | float | | 3 | area to mass ratio | float | | 4 | area | float | | 5 | mass | float | | 6 | velocity | np.array (, 3), containing floats | >*The returned debris is an (n, 7, 3) numpy array. However, only the position and velocity use the third axis as those quanities are vectors.* >*All other fields have 3 copies of their respective data. This was done as a performance optimization for numpy* ## Documentation - [Read the Docs](https://nasa-breakup-model-python.readthedocs.io/en/latest/)
Subscribe above to receive notifications when new versions are released.
VersionDate
Stability
Stability is determined by the version string and my be inaccurate.
0.0.4 Stable
0.0.3 Stable
0.0.2 Stable
0.0.1 Stable