Initial Orbit Determination
Initial Orbit Determination using Least Squares and Extended Kalman Filter
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Initial state vector is computed from three optical sightings using Gauss and Double-R-Iteration methods and then it's optimized applying Least Squares and Extended Kalman Filter.
Cite As
Meysam Mahooti (2026). Initial Orbit Determination (https://www.mathworks.com/matlabcentral/fileexchange/54661-initial-orbit-determination), MATLAB Central File Exchange. Retrieved .
General Information
- Version 1.0.0.0 (1.96 MB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 1.0.0.0 |
