Trans-Lunar Trajectory Optimization - OTB/MICE version
버전 1.0.4 (30.5 MB) 작성자:
David Eagle
Optimization Toolbox version of the tlto_matlab script used to design preliminary lunar missions from Earth park orbit to B-plane encounter.
This submission is a MATLAB script named tlto_matlab_otb that can be used to design preliminary lunar missions from Earth park orbit to B-plane encounter at the moon. The software assumes trans-lunar injection (TLI) occurs impulsively from a circular Earth park orbit. The B-plane coordinates used for targeting the final conditions at the moon are expressed in a moon-centered (selenocentric) mean equator and IAU node of epoch coordinate system. The results from this scientific simulation can be used as an initial guess for a finite-burn trajectory optimization program.
인용 양식
David Eagle (2024). Trans-Lunar Trajectory Optimization - OTB/MICE version (https://www.mathworks.com/matlabcentral/fileexchange/73600-trans-lunar-trajectory-optimization-otb-mice-version), MATLAB Central File Exchange. 검색됨 .
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개발 환경:
R2019b
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- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
- Engineering > Aerospace Engineering > Satellite and Orbital Mechanics >
- Aerospace > Aerospace Toolbox > Standard Workflow Procedures > Coordinate Systems >
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Start Hunting!버전 | 게시됨 | 릴리스 정보 | |
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1.0.4 | Updated several algorithms (apparent sidereal time, sun/moon ephemeris) and the PDF documentation. |
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1.0.3 | Distribution now includes an OTB version (tlto_mice_otb.zip) that uses JPL MICE routines for computing ephemerides. |
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1.0.2 | Added node/apse alignment targeting option. Updated documentation. |
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1.0.1 | Bug fix and documentation update. |
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1.0.0 |