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Iinitial Orbit Determination (Angles-only Method)

version 1.0.1.0 (1.52 MB) by Meysam Mahooti
orbit determination with differential correction

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Updated 14 Mar 2019

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Orbital elements are computed from three sets of right ascension and declination using double-r-iteration method and then they are optimized applying least squares technique.

Cite As

Meysam Mahooti (2019). Iinitial Orbit Determination (Angles-only Method) (https://www.mathworks.com/matlabcentral/fileexchange/55178-iinitial-orbit-determination-angles-only-method), MATLAB Central File Exchange. Retrieved .

Comments and Ratings (4)

Fari Mian

The code is a good effort towards automation of orbit prediction however I cannot make it work for my particular problem. I am using the file "anglesdr.m" file. When I give it the particular inputs, it throws an error which is related to the generation of complex values in "doubler.m". I need help in this regard.
Also there almost no documentation for clarification of variables and functions used in the code.

Demi Moore

Updates

1.0.1.0

Documentation is added.

1.0.0.0

Revised on 2016-11-20.

MATLAB Release Compatibility
Created with R2012b
Compatible with any release
Platform Compatibility
Windows macOS Linux