The problem of control laws, allowing the formation and maintenance of the required halo-orbit, is considered. The motion of the electric propulsion spacecraft is considered in the vicinity of the collinear libration points of the Earth-Moon system. The gravitational effects of the Earth, the Moon and the Sun are taken into account. The results are based on the simplified linearized models of the gravitational potential.
Halo-orbit formation in the Earth-Moon system by the electric propulsion spacecraft
ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia
AIP Conference Proceedings ; 2046 , 1
2018-12-04
8 pages
Conference paper
Electronic Resource
English
An Electric Propulsion Configured Small Halo Orbit...
AIAA | 2005
|Earth-Moon Halo Orbit — Gateway or Tollbooth? (AAS 19-756)
TIBKAT | 2020
|