Physics
Scientific paper
Feb 1989
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989jgcd...12..119p&link_type=abstract
Journal of Guidance, Control, and Dynamics (ISSN 0731-5090), vol. 12, Jan.-Feb. 1989, p. 119-121.
Physics
Earth-Moon Trajectories, Librational Motion, Optimal Control, Spacecraft Motion, Trajectory Optimization, Earth-Moon System, Equations Of Motion, Hamiltonian Functions, Spacecraft Control
Scientific paper
The present treatment of the problem of reaching the collinear and equilateral libration points of the earth-moon system gives attention to the transfer in minimum time of a mass particle initially at rest at the libration point, using a small, constant-magnitude thrust and bounded angular speed to achieve a prescribed final velocity. On this trajectory, the rotation velocity of the direction of the propulsion has the extremal value or corresponds to Lawden's tangent law.
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