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 (the aircraft performance library)

Examples

python simulation.py

python estimate.py --ac B737 --eng CFM56-7B24 --fin data/b737_example_1.csv --noise n3