A MATLAB script for Earth-to-Mars Mission Design - OTB

版本 1.3.0 (16.1 MB) 作者: David Eagle
Optimization Toolbox version of the e2m_matlab script that performs Earth-to-Mars mission analysis and design.
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更新时间 2021/8/7

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PDF document and a MATLAB script named e2m_matlab_otb.m that can be used to design and optimize end-to-end 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.

引用格式

David Eagle (2024). A MATLAB script for Earth-to-Mars Mission Design - OTB (https://www.mathworks.com/matlabcentral/fileexchange/73646-a-matlab-script-for-earth-to-mars-mission-design-otb), MATLAB Central File Exchange. 检索来源 .

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创建方式 R2019b
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版本 已发布 发行说明
1.3.0

Updated script to use the *.bsp ephemeris files. Minor updates to the source code.
1.2.0

Added trajectory verification calculations and updated documentation
1.1.0

Added node/apse targeting. Added additional examples. Updated PDF document.
1.0.1

added "verify optimal solution" calculations
1.0.0