Optimal transfer from collinear libration points with limited rotation speed

Details Optimal transfer from collinear libration points with limited rotation speed Optimal transfer from collinear libration points with limited rotation speed

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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