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Low-energy trajectories to the earth-moon libration points and to halo-orbits impulsive or low-thrust trajectory from an initial circular earth orbit to a given point of this manifold
Route theory for optimal design of satellite constellations to minimize revisit time in low earth orbits of constellation design. In this study route theory for design of constellations for circular low Earth orbits
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
Optimization of flyby schemes in the framework of ADR mission in LEOThe paper focuses on the flyby issue involving large-size space debris (LSSD) objects in low Earth
Electromagnetic background generated by low earth orbit satellites on the earth's surface's surface by mega-constellations of low earth orbit satellites is proposed. Analysis of EMB levels
New research methodology for earth periodic coverage and regularities in parametric localization of optimal low-earth-orbit satellite constellations and localization of optimal low-Earth-orbit satellite constellations parameters are presented and illustrated.
Constellation design for earth periodic coverage in low orbits with minimal satellite swath satellite swath. Possible combinations of satellite orbit parameters and Earth coverage characteristics
ACTIVE SPACE DEBRIS REMOVALthe low-Earth's orbit
Low-Energy Sub-Optimal Low-Thrust Trajectories to Libration Points and Halo-Orbits and calculating a low-thrust trajectory from an initial circular Earth orbit to the given point of this manifold
CHOOSING THE BEST METHOD FOR UTILIZING SPACE DEBRIS IN NEAR-EARTH SPACE and formed in near-Earth space. Based on the known data, an analysis is carried out and a circuit
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