RATIONAL SCHEMES OF CONTROLLED MOTION OF SPACE TETHER SYSTEMS Article Razoumny Y.N., Kupreev S.A. Proceedings of the 4th International Conference on Frontiers of Educational Technologies. ACM New York, NY, USA. 2018. P. 180-185
АНАЛИЗ ВОЗМОЖНОСТЕЙ ПРИМЕНЕНИЯ ДВУХЪЯРУСНЫХ СПУТНИКОВЫХ СИСТЕМ ДЛЯ НЕПРЕРЫВНОГО ОБЗОРА СФЕРИЧЕСКОГО СЛОЯ ОКОЛОЗЕМНОГО КОСМИЧЕСКОГО ПРОСТРАНСТВА Article Разумный Ю.Н., Нгуен Н.К. Системный анализ, управление и навигация. Московский авиационный институт (национальный исследовательский университет). 2017. P. 72-73
METHOD OF TWO-PARAMETERS CONTROL OF SPACECRAFT DURING DESCENT IN THE MARS ATMOSPHERE Article Matyushin M.M., Ovechko V.M., Orlov D.A., Scorobogatov O.P., Tyurina D.D., Razoumny Y.N. Advances in the Astronautical Sciences. Univelt Inc.. 2017. P. 863-872
ESTIMATES OF NEAR-CIRCULAR ORBITS AFTER A SINGLE CORRECTION: A GEOMETRICAL METHOD Article Baranov A.A., Vikhrachev V.O., Karatunov M.O., Razumnyi Y.N. Journal of Computer and Systems Sciences International. Vol. 56. 2017. P. 137-145
ROUTE SATELLITE CONSTELLATIONS FOR EARTH DISCONTINUOUS COVERAGE AND OPTIMAL SOLUTION PECULIARITIES Article Razoumny Y.N. Journal of Spacecraft and Rockets. American Institute of Aeronautics and Astronautics Inc.. Vol. 54. 2017. P. 572-581
GROUND SPACECRAFT CONTROL FACILITIES DISTRIBUTION BY METHOD OF SUCCESSIVE ELIMINATION OF CONFLICTING SITUATIONS Article Matyushin M.M., Ovechko V.M., Polivnikov V.M., Razoumny Y.N., Skorobogatov O.P., Tyurina D.D. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 1065-1075
ГЕОМЕТРИЧЕСКИЙ МЕТОД ОЦЕНКИ ОКОЛОКРУГОВОЙ ОРБИТЫ ПОСЛЕ ОДНОКРАТНОЙ КОРРЕКЦИИ Article Баранов А.А., Вихрачев В.О., Каратунов М.О., Разумный Ю.Н. Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya. 2017. P. 141-149
METHOD OF ENERGY ESTIMATION OF INTERORBITAL TRANSFERS FOR LEO SPACECRAFT ON-ORBIT SERVICING Article Baranov A.A., Razoumny V.Yu., Razoumny Y.N., Malyshev V.V. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 701-709
GROUND SPACECRAFT CONTROL FACILITIES DISTRIBUTION BY METHOD OF SUCCESSIVE ELIMINATION OF CONFLICTING SITUATIONS Article Matyushin M.M., Ovechko V.M., Polivnikov V.M., Skorobogatov O.P., Tyurina D.D., Razoumny Y.N. Advances in the Astronautical Sciences. Univelt Inc.. 2017. P. 1065-1075
LARGE-SIZE SPACE DEBRIS FLYBY IN LOW EARTH ORBITS Article Baranov A.A., Grishko D.A., Razoumny Y.N. Cosmic Research. Maik Nauka Publishing / Springer SBM. Vol. 55. 2017. P. 361-370
SPACECRAFT THRUST VECTOR CONTROL DURING LANDING ON THE MOON SURFACE Article Matyushin M.M., Ovechko V.M., Skorobogatov O.P., Tyurina D.D., Baranova I.S., Razoumny Y.N. Advances in the Astronautical Sciences. Univelt Inc.. 2017. P. 181-188
FLYBY OF LARGE-SIZE SPACE DEBRIS OBJECTS AND THEIR TRANSITION TO THE DISPOSAL ORBITS IN LEO Article Baranov A.A., Grishko D.A., Razoumny Y.N., Jun L. Advances in Space Research. Elsevier Ltd. Vol. 59. 2017. P. 3011-3022
SPACECRAFT GUIDANCE, NAVIGATION AND CONTROL BASED ON APPLICATION OF RESONANT TUNNELING DIODES IN NONLINEAR RADIO SIGNAL CONVERTERS Article Makeev M.O., Meshkov S.A., Sinyakin V.Yu., Razoumny Y.N. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 475-482
DISTURBANCE OBSERVER-BASED FUZZY CONTROL FOR FLEXIBLE SPACECRAFT COMBINED ATTITUDE & SUN TRACKING SYSTEM Article Chak Y.-C., Varatharajoo R., Razoumny Y. Acta Astronautica. Elsevier Ltd. Vol. 133. 2017. P. 302-310
METHOD OF ENERGY ESTIMATION OF INTERORBITAL TRANSFERS FOR LEO SPACECRAFT ON-ORBIT SERVICING Article Baranov A.A., Razoumny V.Y., Razoumny Y.N., Malyshev V.V. Advances in the Astronautical Sciences. Univelt Inc.. 2017. P. 701-709
METHOD OF TWO-PARAMETERS CONTROL OF SPACECRAFT DURING DESCENT IN THE MARS ATMOSPHERE Article Matyushin M.M., Razoumny Y.N., Ovechko V.M., Orlov D.A., Scorobogatov O.P., Tyurina D.D. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 863-872
METHOD OF TETHERED SYSTEM CONTROL FOR DEORBITING OBJECTS USING EARTH'S ATMOSPHERE Article Razoumny Y.N., Kupreev S.A., Misra A.K. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 1031-1050
SPACECRAFT GUIDANCE, NAVIGATION AND CONTROL BASED ON APPLICATION OF RESONANT TUNNELING DIODES IN NONLINEAR RADIO SIGNAL CONVERTERS Article Makeev M.O., Meshkov S.A., Sinyakin V.Y., Razoumny Y.N. Advances in the Astronautical Sciences. Univelt Inc.. 2017. P. 475-482
ON OPTIMIZATION OF TWO-TIER WALKER DELTA PATTERNS SATELLITE CONSTELLATIONS TO PROVIDE CONTINUOUS COVERAGE OF NEAR-EARTH SPACE SPHERICAL LAYER Article Razoumny Y.N., Samusenko O.E., Quy N.N. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 1149-1159
УПРАВЛЕНИЕ ДВИЖЕНИЕМ КОСМИЧЕСКОГО АППАРАТА ПРИ ПОДЛЕТЕ К КРУПНОГАБАРИТНОМУ ОБЪЕКТУ КОСМИЧЕСКОГО МУСОРА Article Баранов А.А., Будянский А.А., Разумный Ю.Н. Космические исследования. Vol. 55. 2017. P. 285-289
SPACECRAFT THRUST VECTOR CONTROL DURING LANDING ON THE MOON SURFACE Article Matyushin M.M., Ovechko V.M., Razoumny Y.N., Skorobogatov O.P., Tyurina D.D., Baranova I.S. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 181-188
THE CONCEPT OF ON-ORBIT-SERVICING FOR NEXT GENERATION SPACE SYSTEM DEVELOPMENT AND ITS KEY TECHNOLOGIES Article Razoumny 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. International Astronautical Federation, IAF. Vol. 16. 2017. P. 10486-10499
ON OPTIMIZATION OF TWO-TIER WALKER DELTA PATTERNS SATELLITE CONSTELLATIONS TO PROVIDE CONTINUOUS COVERAGE OF NEAR-EARTH SPACE SPHERICAL LAYER Article Razoumny Y.N., Samusenko O.E., Quy N.N. Advances in the Astronautical Sciences. Univelt Inc.. 2017. P. 1149-1159
CONTROLLING THE MOTION OF A SPACECRAFT WHEN APPROACHING A LARGE OBJECT OF SPACE DEBRIS Article Baranov A.A., Budyanskiy A.A., Razumnyi Y.N. Cosmic Research. Maik Nauka Publishing / Springer SBM. Vol. 55. 2017. P. 270-274
LOW ORBIT SPACECRAFT SERVICE PLANNING Article Baranov A.A., Razoumny V.Yu., Razoumny Y.N., Malyshev V.V. Proceedings of the International Astronautical Congress, IAC. International Astronautical Federation, IAF. Vol. 2. 2017. P. 835-844