Initial Orbit Determination

Version 1.0.0.0 (1.96 MB) by Meysam Mahooti
Initial Orbit Determination using Least Squares and Extended Kalman Filter
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Updated 29 Dec 2015

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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 .

MATLAB Release Compatibility
Created with R2010a
Compatible with any release
Platform Compatibility
Windows macOS Linux
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Initial Orbit Determination/

Version Published Release Notes
1.0.0.0