Optimal Single Impulse De-orbit from Earth Orbits - OTB
Updated 11 Dec 2019
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).
David Eagle (2021). 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. Retrieved .
MATLAB Release Compatibility
Platform CompatibilityWindows macOS Linux
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!Start Hunting!