Low-Thrust Orbital Transfer with Solar-Electric Propulsion

Versión 1.0.0.0 (46 KB) por David Eagle
orbital transfer using solar-electric propulsion
0.0
(0)
2,5K descargas
Actualizado 30 mar 2016

Ver licencia

This interactive MATLAB script (sep_ltot.m) can be used to determine the characteristics of continuous, low-thrust orbital transfer between two nonplanar circular orbits using solar-electric propulsion (SEP). The numerical method used in this script is described in Chapter 14 of the book Orbital Mechanics by V. Chobotov and the technical paper “The Reformulation of Edelbaum's Low-thrust Transfer Problem Using Optimal Control Theory” by Jean. A. Kechichian, AIAA-92-4576-CP. The original Edelbaum algorithm is described in “Propulsion Requirements for Controllable Satellites”, ARS Journal, August 1961, pp. 1079-1089.

Citar como

David Eagle (2024). Low-Thrust Orbital Transfer with Solar-Electric Propulsion (https://www.mathworks.com/matlabcentral/fileexchange/19757-low-thrust-orbital-transfer-with-solar-electric-propulsion), MATLAB Central File Exchange. Recuperado .

Compatibilidad con la versión de MATLAB
Se creó con R2007a
Compatible con cualquier versión
Compatibilidad con las plataformas
Windows macOS Linux
Categorías
Más información sobre Propulsion Systems en Help Center y MATLAB Answers.

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!

Versión Publicado Notas de la versión
1.0.0.0

BSD update