A MATLAB Script for Computing Hyperbolic Coordinates

This script demonstrates how to compute C3, RLA, and DLA of a hyperbolic orbit.
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Actualizado 29 Jan 2014

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PDF user’s manual and source code for a MATLAB script named demo_hyper that can be used to calculate C3 (twice the specific (per unit mass) orbital energy), RLA (the right ascension) and DLA (declination) of the asymptote of a hyperbolic trajectory. The script can use both Cartesian state vector (position and velocity vectors) and classical orbital elements as the data source.

This computer program assumes that the hyperbolic targets, state vector and classical orbital elements are all in the same Earth-centered-inertial (ECI) coordinate system.

Citar como

David Eagle (2024). A MATLAB Script for Computing Hyperbolic Coordinates (https://www.mathworks.com/matlabcentral/fileexchange/38886-a-matlab-script-for-computing-hyperbolic-coordinates), MATLAB Central File Exchange. Recuperado .

Compatibilidad con la versión de MATLAB
Se creó con R2012b
Compatible con cualquier versión
Compatibilidad con las plataformas
Windows macOS Linux
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Más información sobre Coordinate Systems en Help Center y MATLAB Answers.

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Versión Publicado Notas de la versión
1.1.0.0

Updated user's manual. Added interactive features to the MATLAB script.

1.0.0.0