Single-impulse transfer to a conditionally periodic orbit in the vicinity of the L2 point of the earth-moon system and related problems

Statistics – Computation

Scientific paper

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Earth-Moon System, Lagrangian Equilibrium Points, Spacecraft Motion, Transfer Orbits, Libration, Spacecraft Trajectories, Trajectory Analysis

Scientific paper

The paper examines computational problems connected with spacecraft motion near the L2 Lagrangian equilibrium point. A method is developed for the analysis and calculation of the single-impulse transfer of a spacecraft from an intermediate earth orbit to the conditionally periodic orbit that is most proximate to the L2 point. A numerical assessment is made of the characteristics of the single-parameter correction of the transfer trajectory compensating for the orbit-injection error.

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