Optimal two-impulse transfers to the L2 libration point of the sun-earth system using asymptotic trajectories

Details Optimal two-impulse transfers to the L2 libration point of the sun-earth system using asymptotic trajectories Optimal two-impulse transfers to the L2 libration point of the sun-earth system using asymptotic trajectories

Oct 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991mvsfa..32..102s&link_type=abstract

Moskovskii Universitet, Vestnik, Seriia 3 - Fizika, Astronomiia (ISSN 0579-9392), vol. 32, Sept.-Oct. 1991, p. 102-104. In Russi

Astronomy and Astrophysics

Astronomy

Librational Motion, Solar Neighborhood, Spacecraft Trajectories, Trajectory Optimization, Transfer Orbits, Asymptotic Methods, Celestial Mechanics, Interplanetary Navigation, Runge-Kutta Method

Scientific paper

The paper is concerned with the problem of determining optimal two-impulse transfer trajectories, including transfers to the L2 libration point with and without the use of asymptotic trajectories. It is shown that the use of asymptotic trajectories makes it possible to reduce the energy requirements for a transfer from a near-earth circular satellite orbit to the L2 libration point of the sun-earth system.

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