morbit

Version 1.0.0.0 (2.44 KB) by Russ Sexton
This is a solution for the keplar problem for orbit insertion.
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Updated 29 Dec 1997

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This is a solution for the keplar problem for orbit insertion. Given a burn out velocity and a flight path angle, what is the apogee of the orbit, and the circular orbit that can be achived with one burn at apogee? The delta-velocity for circularization is also plotted. Several other planets , besides earth, are also included and the user can simple adjust the initial parameters to preform orbital analysis of several planets in our home solar system.

Cite As

Russ Sexton (2024). morbit (https://www.mathworks.com/matlabcentral/fileexchange/154-morbit), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R10
Compatible with any release
Platform Compatibility
Windows macOS Linux
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Version Published Release Notes
1.0.0.0