This is orbdetpy, a library of Python and Java routines for orbit determination. It is a thin Python wrapper for our estimation tools and Orekit, which are both written in Java.
The force model for orbit propagation currently includes:
- EGM96 gravity field up to degree and order 360.
- Earth solid tides due to the influence of the Sun and Moon.
- FES 2004 ocean tide model up to degree and order 100.
- The NRL MSISE-00 and simple exponential models for atmospheric drag.
- Solar radiation pressure.
- Third body perturbations from the Sun and Moon.
The measurement model supports range, range-rate, angles, and inertial Cartesian coordinates. Filtering is done using Orekit's Extended Kalman Filter or our custom Unscented Kalman Filter. Dynamic Model Compensation (DMC) can be used with either filter to estimate additional perturbing acclerations that result from unmodeled dynamics, maneuvers etc.
You can either use your own measurements or simulate observations using
- Install the Java Development Kit 8 (1.8) from http://openjdk.java.net/install/index.html. Set the JAVA_HOME environment variable to point to your JDK installation.
- Install Python 3.6+ and run
pip install orbdetpyto install orbdetpy and other package dependencies from the Python Package Index (PyPI). If you wish to use the
developor other experimental branches from GitHub,
git clonethem and run
pip install -e .from the top level
- Source code, example programs and data files can be downloaded from https://github.com/ut-astria/orbdetpy.
The orbdetpy/lib folder contains JAR files for the following libraries, which are imported by orbdetpy automatically.
Update the astrodynamics data in orbdetpy/data periodically by calling
update_data() function in the
The following example programs can be found in the 'examples' folder. These examples use the Python wrapper interface but calling the underlying Java implementation directly is straightforward.
testsim.py: Demonstrates the measurement simulator. Note that maneuvers can be incorporated into the force model during simulation.
plotsim.py: Plots the results of simulations created using testsim.py.
testodet.py: Demonstrates orbit determination in orbdetpy.
plotodet.py: Plots the results of fitting orbits using testodet.py.
run_tests.py: Run all the use cases under examples/data. Simulated measurements, orbit fits, differences between simulated truth versus estimates, and 3-sigma of estimated covariances will be written to output/ sub-folders.
orbdetpy uses JSON files to store settings, measurements and estimation results. The files in examples/data show how to configure measurement simulation and orbit determination using radar or telescope data. The file docs/file_formats.md documents the structure of the JSON files.
The following are some typical use cases. It is assumed that the current working directory is examples/data.
Simulate state vectors and radar measurements:
python ../testsim.py radar_sim_cfg.json sim_data.json
This will run the simulation configured in radar_sim_cfg.json and write simulated output to sim_data.json.
Plot simulation results:
python ../plotsim.py radar_sim_cfg.json sim_data.json
This will plot the simulated data generated in (1).
Run OD on simulated radar data:
python ../testodet.py radar_od_cfg.json sim_data.json od_output.json
This will run OD on the simulated radar data generated in (1) using the OD configuration in radar_od_cfg.json and write OD output to od_output.json.
Plot OD results:
python ../plotodet.py radar_od_cfg.json sim_data.json od_output.json
This will plot the OD results from (3).
Java "Out of heap space" errors:
The Java Virtual Machine with default settings may run out of heap space during long term simulations or orbit fits. The workaround is to add the following to the top of your Python code, before orbdetpy is imported. The value following "-Xmx" is the maximum heap size you wish to assign to Java; "G" stands for gigabytes.