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A MATLAB Script for Earth-to-Mars Mission Design

version 1.4.0.0 (106 KB) by David Eagle
Determines optimal n-body ballistic trajectories from Earth park orbit to encounter at Mars.

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Updated 17 Apr 2018

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PDF document and a MATLAB script named e2m_matlab.m that can be used to design and optimize ballistic interplanetary missions from Earth park orbit to encounter at Mars. The software assumes that interplanetary injection occurs impulsively from a circular Earth park orbit. The B-plane coordinates are expressed in a Mars-centered (areocentric) mean equator and IAU node of epoch coordinate system. B-plane targets are enforced using either a combination of periapsis radius and orbital inclination, individual B-plane coordinates of the arrival hyperbola, or entry interface (EI) conditions at Mars. The type of targeting and the target values are defined by the user.

Comments and Ratings (4)

maybe the e2m_readdata.m has some problems

sun Chong

Updates

1.4.0.0

Updated MATLAB keywords (strfind, etc.) and DT data file. Minor editing of the MATLAB source code for clearer data display, etc.

1.3.0.0

Updated e2m_matlab.m main script to use 64bit, September, 2014 version of SNOPT. Also updated input data files.

1.2.0.0

UPDATED LINKS

SNOPT ccom.ucsd.edu/~optimizers/

Binary Ephemeris Files

https://www.dropbox.com/sh/hul0g7ia6nhspwo/AAATqfVXb5ClZODfGGvEbRZEa?dl=0

1.1.0.0

Added main script file (e2m_matlab_64bit.m) that uses the March 17, 2014 version of SNOPT.

MATLAB Release Compatibility
Created with R2018a
Compatible with any release
Platform Compatibility
Windows macOS Linux