Concerning the optimal transfer of space vehicles at equidistant libration points in the earth-moon system

Details Concerning the optimal transfer of space vehicles at equidistant libration points in the earth-moon system Concerning the optimal transfer of space vehicles at equidistant libration points in the earth-moon system

Feb 1980

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980stcma..39...29p&link_type=abstract

Studii si Cercetari de Mecanica Aplicata, vol. 39, Jan.-Feb. 1980, p. 29-47. In Rumanian.

Astronomy and Astrophysics

Astronomy

Astrodynamics, Earth-Moon System, Lagrangian Equilibrium Points, Spacecraft Trajectories, Trajectory Optimization, Transfer Orbits, Differential Equations, Euler-Lagrange Equation, Fuel Consumption, Libration

Scientific paper

The optimal trajectory is determined for the transferring of space
vehicles at equidistant libration points in the earth-moon system with a
minimum consumption of fuel. The rigorous presentation includes the
integration of Lagrange's equations, laws of optimal motions, and the
determination of extrema.

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