Physics
Scientific paper
Feb 1994
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1994kosis..32q...3l&link_type=abstract
Kosmicheskie Issledovaniia, Tom 32, Vyp. 1, p. 3 - 35
Physics
Artificial Satellites: Orbit Theory, Artificial Satellites: Motion
Scientific paper
The authors describe an approximate analytical method for calculating the motion of a spacecraft near the libration points L1, L2 for an arbitrary system of bodies. In connection with trajectory problems with the "Relikt-2" project (halo-orbit in the vicinity of the L2 point of the Sun-Earth system) the lunar perturbations were also taken into account. The problem of screening of a spacecraft in a halo-orbit by the Earth from solar radiation is discussed. An analytical method was used for correcting spacecraft motion in order to prevent screening.
Lidov M. L.
Lyakhova V. A.
Vashkov'yak M. A.
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