ON OPTIMIZATION OF TWO-TIER WALKER DELTA PATTERNS SATELLITE CONSTELLATIONS TO PROVIDE CONTINUOUS COVERAGE OF NEAR-EARTH SPACE SPHERICAL LAYER ArticleRazoumny Y.N., Samusenko O.E., Quy N.N.Advances in the Astronautical Sciences. Том 161. 2017. С. 1149-1159
АНАЛИЗ ВОЗМОЖНОСТЕЙ ПРИМЕНЕНИЯ ДВУХЪЯРУСНЫХ СПУТНИКОВЫХ СИСТЕМ ДЛЯ НЕПРЕРЫВНОГО ОБЗОРА СФЕРИЧЕСКОГО СЛОЯ ОКОЛОЗЕМНОГО КОСМИЧЕСКОГО ПРОСТРАНСТВА ArticleРазумный Ю.Н., Нгуен Н.К.Системный анализ, управление и навигация. 2017. С. 72-73
ESTIMATES OF NEAR-CIRCULAR ORBITS AFTER A SINGLE CORRECTION: A GEOMETRICAL METHOD ArticleBaranov A.A., Vikhrachev V.O., Karatunov M.O., Razumnyi Y.N.Journal of Computer and Systems Sciences International. Том 56. 2017. С. 137-145
METHOD OF ENERGY ESTIMATION OF INTERORBITAL TRANSFERS FOR LEO SPACECRAFT ON-ORBIT SERVICING ArticleBaranov A.A., Razoumny V.Yu., Razoumny Y.N., Malyshev V.V.Advances in the Astronautical Sciences. Том 161. 2017. С. 701-709
LARGE-SIZE SPACE DEBRIS FLYBY IN LOW EARTH ORBITS ArticleBaranov A.A., Grishko D.A., Razoumny Y.N.Cosmic Research. Том 55. 2017. С. 361-370
GROUND SPACECRAFT CONTROL FACILITIES DISTRIBUTION BY METHOD OF SUCCESSIVE ELIMINATION OF CONFLICTING SITUATIONS ArticleMatyushin M.M., Ovechko V.M., Polivnikov V.M., Razoumny Y.N., Skorobogatov O.P., Tyurina D.D.Advances in the Astronautical Sciences. Том 161. 2017. С. 1065-1075
METHOD OF TWO-PARAMETERS CONTROL OF SPACECRAFT DURING DESCENT IN THE MARS ATMOSPHERE ArticleMatyushin M.M., Razoumny Y.N., Ovechko V.M., Orlov D.A., Scorobogatov O.P., Tyurina D.D.Advances in the Astronautical Sciences. Том 161. 2017. С. 863-872
DISTURBANCE OBSERVER-BASED FUZZY CONTROL FOR FLEXIBLE SPACECRAFT COMBINED ATTITUDE & SUN TRACKING SYSTEM ArticleChak Y.-C., Varatharajoo R., Razoumny Y.Acta Astronautica. Том 133. 2017. С. 302-310
THE CONCEPT OF ON-ORBIT-SERVICING FOR NEXT GENERATION SPACE SYSTEM DEVELOPMENT AND ITS KEY TECHNOLOGIES ArticleRazoumny Y.N., Spencer D.B., Agrawal B., Kreisel J., Yasaka T., Koupreev S.A., Razoumny V., Makarov Y.Proceedings of the International Astronautical Congress, IAC. Том 16. 2017. С. 10486-10499
FLYBY OF LARGE-SIZE SPACE DEBRIS OBJECTS AND THEIR TRANSITION TO THE DISPOSAL ORBITS IN LEO ArticleBaranov A.A., Grishko D.A., Razoumny Y.N., Jun L.Advances in Space Research. Том 59. 2017. С. 3011-3022
FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 3: LOW-COST EARTH OBSERVATION WITH MINIMAL SATELLITE SWATH ArticleRazoumny Y.N.Acta Astronautica. Том 129. 2016. С. 447-458
EMULATING OF THE STATIONARY OBSERVATION OF THE EARTH LOCAL REGION USING LOCALLY GEOSTATIONARY ELLIPTIC ORBITS ArticleRazoumny Y.N.Advances in the Astronautical Sciences. Том 158. 2016. С. 2933-2943
FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 4: COMPOUND SATELLITE STRUCTURES ON ORBITS WITH SYNCHRONIZED NODAL REGRESSION ArticleRazoumny Y.N.Acta Astronautica. Том 129. 2016. С. 459-465
FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 2: SYNTHESIS OF SATELLITE ORBITS AND CONSTELLATIONS ArticleRazoumny Y.N.Acta Astronautica. Том 128. 2016. С. 741-758
FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 1: ANALYTIC EMULATION OF THE EARTH COVERAGE ArticleRazoumny Y.N.Acta Astronautica. Том 128. 2016. С. 722-740