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.
Nishant Gupta (2020). 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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