https://github.com/junzis/acsmc
Aircraft mass estimator based on sequential Monte Carlo method
https://github.com/junzis/acsmc
Last synced: 4 months ago
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Aircraft mass estimator based on sequential Monte Carlo method
- Host: GitHub
- URL: https://github.com/junzis/acsmc
- Owner: junzis
- License: agpl-3.0
- Created: 2019-02-18T22:26:12.000Z (over 6 years ago)
- Default Branch: master
- Last Pushed: 2019-02-19T23:32:52.000Z (over 6 years ago)
- Last Synced: 2025-01-30T02:51:06.610Z (4 months ago)
- Language: Python
- Homepage:
- Size: 857 KB
- Stars: 4
- Watchers: 3
- Forks: 1
- Open Issues: 0
-
Metadata Files:
- Readme: README.md
- License: LICENSE
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README
# Aircraft state estimation
## The Sequential Monte Carlo (a.k.a. particle filter)
The repository implements a particle filter for aircraft mass and thrust setting estimation base on the point-mass aircraft performance model. It can also be used for other state filtering.
## Required library
- [OpenAP](https://github.com/junzis/openap) (the aircraft performance library)
## Examples
```sh
python simulation.py
python estimate.py --ac B737 --eng CFM56-7B24 --fin data/b737_example_1.csv --noise n3
```