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SOLUTION OF THE EULER-LAMBERT PROBLEM BY THE OKHOTSIMSKY-EGOROV METHOD. Thus, the solution boils down to determining the angle of inclination of the speed corresponding to a
Extension of the Kepler problem towards minimization of energy and gravity softeningThe classical Kepler Problem consists in the determination of the relative orbital motion of a
The effectiveness of orbital volumes calculations after traumatic injuries based on CT data and lateral walls of the right orbit. In order to determine further treatment tactics for this patient (sur
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
Method for determining the moments of trajectory measurements for the correction of the accumulating orbit shift of the spacecraft of measurement moments to eliminate the accumulating shift along the orbit. The method is based
Assessment of Non-Coplanar Maneuver Parameters and Perturbing Accelerations Using the Minimal Number of Observations and is active throughout the whole time interval from the moment of the last orbit determination to the moment
АЛГОРИТМ РЕШЕНИЯ ЗАДАЧИ ЭЙЛЕРА-ЛАМБЕРТА НА ОСНОВЕ МЕТОДА ОХОЦИМСКОГО-ЕГОРОВА, it was possible to obtain a new orbit determination method. The advantages of this method are the limitation
Electronic chemical potential and orbital electronegativity of univalent substituents in the ground state and the orbital chemical potential of its valence state, the latter being equal in absolute
Orbital dynamics of a binary system composed of a massive star and a black hole companion. By monitoring the mass transfer from the star to the black hole, we perform a thorough and systematic orbit
Low thrust transfers to space debris object neighborhood-eccentricity non-coplanar orbits is considered. The transfer period is divided into two intervals. Each interval
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