Resonance effects during low-thrust motion in the earth-moon system

Details Resonance effects during low-thrust motion in the earth-moon system Resonance effects during low-thrust motion in the earth-moon system

May 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987kosis..25..374k&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 25, May-June 1987, p. 374-383. In Russian.

Physics

1

Earth-Moon Trajectories, Low Thrust, Orbit Perturbation, Resonance, Satellite Orbits, Three Body Problem, Asymptotic Methods, Orbital Resonances (Celestial Mechanics), Spacecraft Trajectories

Scientific paper

During low-thrust acceleration or deceleration in the earth's sphere of influence, the osculating period of the spacecraft revolution can have values that are rationally commensurate with the moon's revolution period. This leads to the problem of orbital resonances, which, under certain conditions, can produce a qualitative change in the pattern of spacecraft motion including capture in stable resonance. An analytical expression is obtained for these conditions; and examples of asymptotically stable resonant orbits are considered for acceleration with tangential thrust.

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