Razoumny Y.N. - list of publications

THE RESEARCH METHOD OF CONTROLLED MOVEMENT DYNAMICS OF TETHER SYSTEM

Article

Razoumny Y.N., Kupreev S.A., Misra A.K.

Advances in the Astronautical Sciences. Univelt Inc.. Vol. 170. 2020. P. 417-431

ON THE MOTION OF BODIES BASED ON CHANGES IN THE KINETIC MOMENT

Article

Razoumny Y.N., Kupreev S.A.

RUDN Journal of Engineering Researches. Федеральное государственное автономное образовательное учреждение высшего образования Российский университет дружбы народов (РУДН). Vol. 20. 2019. P. 267-275

LOCALLY GEOSTATIONARY ORBITS: OPTIMAL GEOMETRY OF ELLIPTIC ORBIT FOR EARTH COVERAGE

Article

Razoumny Y.N.

Journal of Spacecraft and Rockets. American Institute of Aeronautics and Astronautics Inc.. Vol. 56. 2019. P. 1017-1023

SATELLITE CONSTELLATION DESIGN OF ON-ORBIT SERVICING SPACE SYSTEM FOR GLOBALSTAR SATELLITES

Article

Razoumny V.Y., Baranov A.A., Razoumny Y.N.

RUDN Journal of Engineering Researches. Федеральное государственное автономное образовательное учреждение высшего образования Российский университет дружбы народов (РУДН). Vol. 20. 2019. P. 111-122

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

FLOWER CONSTELLATIONS FOR EARTH COVERAGE WITH BIG NUMBER OF SATELLITES

Article

Lee S., Avendano M.E., Razoumny Y., Mortari D.

Proceedings of the International Astronautical Congress, IAC. International Astronautical Federation, IAF. Vol. 2018-October. 2018.

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

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

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

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

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

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

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

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

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

Разумный Ю.Н.

List of records

THE RESEARCH METHOD OF CONTROLLED MOVEMENT DYNAMICS OF TETHER SYSTEM

ON THE MOTION OF BODIES BASED ON CHANGES IN THE KINETIC MOMENT

LOCALLY GEOSTATIONARY ORBITS: OPTIMAL GEOMETRY OF ELLIPTIC ORBIT FOR EARTH COVERAGE

SATELLITE CONSTELLATION DESIGN OF ON-ORBIT SERVICING SPACE SYSTEM FOR GLOBALSTAR SATELLITES

RATIONAL SCHEMES OF CONTROLLED MOTION OF SPACE TETHER SYSTEMS

FLOWER CONSTELLATIONS FOR EARTH COVERAGE WITH BIG NUMBER OF SATELLITES

SPACECRAFT GUIDANCE, NAVIGATION AND CONTROL BASED ON APPLICATION OF RESONANT TUNNELING DIODES IN NONLINEAR RADIO SIGNAL CONVERTERS

METHOD OF TWO-PARAMETERS CONTROL OF SPACECRAFT DURING DESCENT IN THE MARS ATMOSPHERE

FLYBY OF LARGE-SIZE SPACE DEBRIS OBJECTS AND THEIR TRANSITION TO THE DISPOSAL ORBITS IN LEO

ГЕОМЕТРИЧЕСКИЙ МЕТОД ОЦЕНКИ ОКОЛОКРУГОВОЙ ОРБИТЫ ПОСЛЕ ОДНОКРАТНОЙ КОРРЕКЦИИ

ESTIMATES OF NEAR-CIRCULAR ORBITS AFTER A SINGLE CORRECTION: A GEOMETRICAL METHOD

GROUND SPACECRAFT CONTROL FACILITIES DISTRIBUTION BY METHOD OF SUCCESSIVE ELIMINATION OF CONFLICTING SITUATIONS

SPACECRAFT THRUST VECTOR CONTROL DURING LANDING ON THE MOON SURFACE

SPACECRAFT THRUST VECTOR CONTROL DURING LANDING ON THE MOON SURFACE

LARGE-SIZE SPACE DEBRIS FLYBY IN LOW EARTH ORBITS

Other authors

Друшляков С.С.

Evtushenko O.N.