Initial Orbit Determination
Version 1.0.0.0 (1.96 MB) by
Meysam Mahooti
Initial Orbit Determination using Least Squares and Extended Kalman Filter
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 (2024). 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
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Initial Orbit Determination/
Version | Published | Release Notes | |
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1.0.0.0 |