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Low Thrust Transfer Between Non-coplanar Circular Orbits

version (831 KB) by David Eagle
Design and analyze low-thrust orbit transfers


Updated 23 Oct 2013

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PDF document and MATLAB script named ltot.m that can be used to determine the characteristics of low-thrust orbital transfer between two non-coplanar circular orbits. The algorithm used in this script is based on Edelbaum’s method which 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 J. A. Kechichian, AIAA-92-4576-CP. The original Edelbaum algorithm is described in “Propulsion Requirements for Controllable Satellites”, ARS Journal, August 1961, pages 1079-1089.

Cite As

David Eagle (2020). Low Thrust Transfer Between Non-coplanar Circular Orbits (, MATLAB Central File Exchange. Retrieved .

Comments and Ratings (5)

ahmet burak koç


Thanks very much for the document, it's concise, clear and beautiful !

mostafa mohammadi

sun Chong

Zaw Min Tun

MATLAB Release Compatibility
Created with R2012a
Compatible with any release
Platform Compatibility
Windows macOS Linux