Updated 04 Apr 2020
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.
David Eagle (2020). A MATLAB script for Earth-to-Mars Mission Design (https://www.mathworks.com/matlabcentral/fileexchange/74671-a-matlab-script-for-earth-to-mars-mission-design), MATLAB Central File Exchange. Retrieved .
Added trajectory verification calculations and updated documentation