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New orbits of wide visual double stars the orbits of ten wide visual double stars by the apparent motion parameter method. The orientation
New orbits of wide visual double stars the orbits of ten wide visual double stars by the apparent motion parameter method. The orientation
Estimates of near-circular orbits after a single correction: a geometrical method and numerical-analytical algorithms to estimate short-term and long-term one-impulse maneuvers for the case
Diamond-like carbon coatings to protect the optical surfaces of orbital telescopes from the outer space factors with an electric arc method with laser burning of a carbon plasma and separation of the cloud of plasma. Describes
Two-impulse orbital transfer based on the solution of Lambert problem with optimal flight time, it is assumed that the orbit that connects two given positions is a flight trajectory, the costs of which
Emulating of the stationary observation of the Earth local region using locally geostationary elliptic orbitsThe problem of optimization of the satellite orbits for local Earth coverage is considered
Nonlinearity in inverse problems of the dynamics of Jupiter’s outer satellites problems of the dynamics of Jupiter’s Outer Satellites, observed on very short orbital arcs
Evaluation of impulsive maneuvers performed by active space object-Analytical algorithms of estimating one-pulse and two-pulse maneuvers of short duration are proposed. Both coplanar
Analysis of orbital theories for the construction of the numerical theory of the lunar physical librations and analytical theories of lunar orbital motion. During these studies, the impact on the parameters of physical
Optimal formation and replenishment of lunar satellite constellations. It is supposed that the orbital inclination was formed during the transfer to the orbit around the Moon
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