A MATLAB Script for Designing Interplanetary Launch Trajectories

版本 1.0.0.0 (362.4 KB) 作者: David Eagle
Preliminary design and analysis of interplanetary launch trajectories.
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更新时间 2012/11/12

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This MATLAB script determines the launch universal time, orbital elements of the departure hyperbola, injection delta-v, and estimates park orbit coast times for both short and long coast injection opportunities. This information can be used to create initial guesses for other trajectory simulations.

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David Eagle (2024). A MATLAB Script for Designing Interplanetary Launch Trajectories (https://www.mathworks.com/matlabcentral/fileexchange/39008-a-matlab-script-for-designing-interplanetary-launch-trajectories), MATLAB Central File Exchange. 检索来源 .

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版本 已发布 发行说明
1.0.0.0