Circular-Restricted Three-Body Problem (CRTBP) - Sun_Earth_Moon

Version 1.0.0.0 (1.37 KB) by Nishant Gupta
Simulation the Hill’s Problem of 3-body system in MATLAB
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Updated 23 Jan 2011

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Analysis and simulation of orbits in circular-restricted three-body problem (CRTBP), where primary and secondary bodies move in circular orbits about the common center of mass, and effect of gravitational attraction of the smallest body are ignored. The applications described here are for orbital problems in the Sun-Earth-Moon system,whose trajectory was simulated in MATLAB.

Cite As

Nishant Gupta (2024). Circular-Restricted Three-Body Problem (CRTBP) - Sun_Earth_Moon (https://www.mathworks.com/matlabcentral/fileexchange/30135-circular-restricted-three-body-problem-crtbp-sun_earth_moon), MATLAB Central File Exchange. Retrieved .

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Created with R2010a
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Version Published Release Notes
1.0.0.0