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
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
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