Modeling Rocket Ascent from the Moon

版本 1.0.0 (835.1 KB) 作者: David Eagle
Model the launch of a single-stage rocket-propelled vehicle from the surface of the Moon.
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更新时间 2025/3/13

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This submission is a MATLAB script named demo_lunar_ascent that demonstrates how to model a single-stage, finite-burn lunar ascent trajectory. The trajectory is modeled as a user-defined vertical rise phase, a pitch-over phase and a finite-burn ascent-to-orbit phase. The optimal flight controls (angle-of-attack, bank angle and throttle setting) for this script are computed using the lascent_sos computer program.
Additional information about the lascent_sos program can be found in Appendix B of this document.
The important features of this MATLAB script are as follows:
  • user-defined vertical rise and pitch-over phases
  • angle-of-attack, bank angle and throttle control variables
  • 3-DOF flight path equations of motion relative to a spherical, rotating Moon
  • user-defined vehicle mass and propulsion properties

引用格式

David Eagle (2025). Modeling Rocket Ascent from the Moon (https://ww2.mathworks.cn/matlabcentral/fileexchange/180369-modeling-rocket-ascent-from-the-moon), MATLAB Central File Exchange. 检索时间: .

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版本 已发布 发行说明
1.0.0