Optimal trajectories in the transfer problem of space vehicles from Lagrangian collinear points

Details Optimal trajectories in the transfer problem of space vehicles from Lagrangian collinear points Optimal trajectories in the transfer problem of space vehicles from Lagrangian collinear points

Oct 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991mont.iafcv....p&link_type=abstract

IAF, International Astronautical Congress, 42nd, Montreal, Canada, Oct. 5-11, 1991. 8 p.

Astronomy and Astrophysics

Astronomy

Lagrangian Equilibrium Points, Lunar Trajectories, Trajectory Optimization, Transfer Orbits, Collinearity, Command Guidance, Earth-Moon System, Equations Of Motion, Extremum Values, Fuel Consumption, Libration, Mayer Problem

Scientific paper

The present paper illustrates the study of transfering the space vehicles from the collinear libration points of the earth-moon system to the maximum distance, assuming that the evolution time is known. After the analysis of the admissible states, the optimal command law which represents the absolute extremum in a class of relative extrema is determined.

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