Lunar Free-Return Trajectory Analysis with MATLAB
The system dynamics are modeled as a simplified circular-restricted three-body problem (CRTBP). Additional modeling assumptions are (1)the massless third body is subject only to the point-mass gravity of the earth and moon (2) the moon is subject only to the point mass gravity of the earth (3) the moon’s orbit is circular and all motion lies in the moon’s orbital plane (4) departure from the earth park orbit is the counterclockwise direction (5) trans-lunar injection (TLI) occurs impulsively from a circular earth park orbit (6) the TLI departure maneuver is applied tangential to the earth park orbit (7) the earth orbit insertion (EOI) impulsive maneuver is applied tangential to the return trajectory (8) the lunar flyby is a no maneuver, ballistic trajectory.
引用格式
David Eagle (2024). Lunar Free-Return Trajectory Analysis with MATLAB (https://www.mathworks.com/matlabcentral/fileexchange/45710-lunar-free-return-trajectory-analysis-with-matlab), MATLAB Central File Exchange. 检索来源 .
MATLAB 版本兼容性
平台兼容性
Windows macOS Linux类别
标签
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!