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Optimal formation and replenishment of lunar satellite constellations orbit. The precession velocity and revolution period of this orbit differ from the parameters of future

Radiology of postoperative period in patients with orbital trauma period with orbital volumes were reconstructed and symmetrical compared to the other side in 48 patients

Method for constellation design for earth periodic coverage using compound satellite structures on orbits with synchronized nodal regressionThe problem of optimization of the satellite orbits and constellations for Earth periodic coverage

Modern capabilities of the computed tomography in orbital traumatic injuries diagnosis position and of changes in the density of the orbital soft tissues. RESULTS: In the preoperative period

Route theory for optimal design of satellite constellations to minimize revisit time in low earth orbits for continuous and periodical coverage are principally differed by orbit parameters as well as by methods

Trajectories Derived from Periodic Orbits around the Lagrangian Point L1 and Lunar Swing-Bys: Application in Transfers to Near-Earth AsteroidsTo present a set of trajectories derived from the retrograde periodic orbits around the Lagrangian

New methods for CT data analysis in patients with posttraumatic defects and deformations of the midface, to develop the methods for post-processing of CT data in patients with orbital injury in order to obtain

Periodic orbits in the restricted three-body problem for observations of the smaller primaryPeriodic orbits in the restricted three-body problem for observations of the smaller primary

Stability of Periodic Solutions for Hysteresis-Delay Differential Equations established existence and uniqueness of solutions, we focus on the analysis of stability of periodic solutions

On the Floquet multipliers of periodic solutions to non-linear functional differential equations orbits which are unstable and hyperbolic. An example of a non-autonomous periodic linear delay

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