Optimal Single Impulse De-orbit from Earth Orbits - OTB

Version 1.0.0 (624 ko) par David Eagle
Optimization Toolbox version of the deorbit.m MATLAB script which determines optimal de-orbit maneuvers.
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Mise à jour 11 déc. 2019

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This document describes a MATLAB script named deorbit_otb that can be used to compute the single optimal impulsive maneuver required to de-orbit a spacecraft in a circular or elliptical Earth orbit. The user provides the classical orbital elements of the initial orbit along with the desired geodetic altitude and relative flight path angle targets at the entry interface (EI).

Citation pour cette source

David Eagle (2024). Optimal Single Impulse De-orbit from Earth Orbits - OTB (https://www.mathworks.com/matlabcentral/fileexchange/73645-optimal-single-impulse-de-orbit-from-earth-orbits-otb), MATLAB Central File Exchange. Récupéré le .

Compatibilité avec les versions de MATLAB
Créé avec R2019b
Compatible avec toutes les versions
Plateformes compatibles
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Version Publié le Notes de version
1.0.0