Physics
Scientific paper
Mar 1991
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991kosis..29..247i&link_type=abstract
Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 29, Mar.-Apr. 1991, p. 247-254. In Russian.
Physics
Circular Orbits, Earth-Mars Trajectories, Interplanetary Navigation, Spacecraft Trajectories, Gravitational Fields, Trajectory Optimization
Scientific paper
A method is proposed for navigation in the zone of approach to Mars, using relative measurements in the two-object system: the satellite and a mobile reference object (such as a detachable satellite probe or a descending device). The method can be used for inserting a satellite into a Martian orbit. Results are presented of numerical simulations of navigation in this zone in the presence of perturbation effects.
Ivankov Petr R.
Ivanov Nikolai M.
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