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Spacecraft thrust vector control during landing on the moon surface and soft landing from the circular satellite orbit of the Moon to its surface, is considered. The maximum
Four methods for determining intermediate perturbed orbits from three observations: a comparisonTheoretical and numerical comparison of four methods for determining the orbit of a small celestial
Near-horizon circular orbits and extremal limit for dirty rotating black holes" (surrounded by matter) black holes. Near-horizon circular equatorial orbits are examined in two different
Solution of the Euler–Lambert Problem Based on the Okhotsimsky–Egorov Ballistic Approach method for determining the orbit corresponding to a given flight time. It is logical to name
Manifold dynamics and periodic orbits in a multiwell potential that determine the escapes from a multiwell potential. We also present the network of both symmetric
Stability of Periodic Solutions for Hysteresis-Delay Differential Equations prove that the spectrum of this formal linearization determines the stability of the periodic solution
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
Monte Carlo modeling of spin FETs controlled by spin-orbit interaction in the Monte Carlo method to account for the spin polarization dynamics. The spin-orbit interaction in the spin
МЕТОД ОХОЦИМСКОГО-ЕГОРОВА ДЛЯ РЕШЕНИЯ ЗАДАЧИ ЭЙЛЕРА-ЛАМБЕРТА.E. Okhotsimsky and on the analysis of a set of orbits for flight between two given points in the central
Genetic analysis of parameters of near earth asteroids for determining parent bodies of meteoroid streams© 2017 COSPAR. The present paper is focusing on determining genetic connections between small
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