Razoumny Y.N. - list of publications

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

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

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

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

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

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

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

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

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

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

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

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

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

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

METHOD FOR CONSTELLATION DESIGN FOR EARTH PERIODIC COVERAGE USING COMPOUND SATELLITE STRUCTURES ON ORBITS WITH SYNCHRONIZED NODAL REGRESSION

Article

Razoumny Y.N.

Advances in the Astronautical Sciences. Univelt Inc.. Vol. 158. 2016. P. 2965-2979

FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 2: SYNTHESIS OF SATELLITE ORBITS AND CONSTELLATIONS

Article

Razoumny Y.N.

Acta Astronautica. Elsevier Ltd. Vol. 128. 2016. P. 741-758

FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 4: COMPOUND SATELLITE STRUCTURES ON ORBITS WITH SYNCHRONIZED NODAL REGRESSION

Article

Razoumny Y.N.

Acta Astronautica. Elsevier Ltd. Vol. 129. 2016. P. 459-465

EMULATING OF THE STATIONARY OBSERVATION OF THE EARTH LOCAL REGION USING LOCALLY GEOSTATIONARY ELLIPTIC ORBITS

Article

Razoumny Y.N.

Advances in the Astronautical Sciences. Univelt Inc.. Vol. 158. 2016. P. 2933-2943

FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 3: LOW-COST EARTH OBSERVATION WITH MINIMAL SATELLITE SWATH

Article

Razoumny Y.N.

Acta Astronautica. Elsevier Ltd. Vol. 129. 2016. P. 447-458

METHOD OF OPTIMIZATION OF THE SERVICING SPACE-BASED SYSTEM ORBITS AND DETACHED UNITS MANEUVERES PARAMETERS IN THE PROBLEM OF ON-ORBIT-SERVICING OF THE GIVEN MULTI-SATELLITE SPACE INFRASTRUCTURE

Article

Razoumny Y., Baranov A., Razoumny V., Varatharajoo R., Kozlov P.

Proceedings of the International Astronautical Congress, IAC. International Astronautical Federation, IAF. 2016.

FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 1: ANALYTIC EMULATION OF THE EARTH COVERAGE

Article

Razoumny Y.N.

Acta Astronautica. Elsevier Ltd. Vol. 128. 2016. P. 722-740

О ВНЕДРЕНИИ СОВРЕМЕННЫХ ТЕХНОЛОГИЙ УПРАВЛЕНИЯ ИННОВАЦИОННЫМИ ПРОЕКТАМИ

Article

Шкваря Л.В., Разумный Ю.Н., Евтушенко О.Н., Семенов А.С.

Экономика и предпринимательство. Редакция журнала Экономика и предпринимательство. 2015. P. 822-824

МНОГОКРИТЕРИАЛЬНЫЙ ПОДХОД К ЗАДАЧЕ ВЫБОРА ЭФФЕКТИВНОГО ИННОВАЦИОННОГО ПРОЕКТА

Article

Чурсин А.А., Разумный Ю.Н., Мильковский А.Г., Корнеенко В.П.

Микроэкономика. Акционерное общество Институт микроэкономики. 2015. P. 6-13

МОДЕЛЬ ОЦЕНКИ РИСКОВ В ПРОИЗВОДСТВЕ ВЫСОКОТЕХНОЛОГИЧНОЙ ПРОДУКЦИИ И ОЦЕНКА ИХ ВЛИЯНИЯ НА РОСТ СЕБЕСТОИМОСТИ И ЦЕНЫ

Article

Чурсин А.А., Разумный Ю.Н., Шамин Р.В., Анфимова М.Л.И

Экономика и предпринимательство. Редакция журнала Экономика и предпринимательство. 2015. P. 682-688

Разумный Ю.Н.

List of records

LARGE-SIZE SPACE DEBRIS FLYBY IN LOW EARTH ORBITS

METHOD OF ENERGY ESTIMATION OF INTERORBITAL TRANSFERS FOR LEO SPACECRAFT ON-ORBIT SERVICING

THE CONCEPT OF ON-ORBIT-SERVICING FOR NEXT GENERATION SPACE SYSTEM DEVELOPMENT AND ITS KEY TECHNOLOGIES

ГЕОМЕТРИЧЕСКИЙ МЕТОД ОЦЕНКИ ОКОЛОКРУГОВОЙ ОРБИТЫ ПОСЛЕ ОДНОКРАТНОЙ КОРРЕКЦИИ

SPACECRAFT THRUST VECTOR CONTROL DURING LANDING ON THE MOON SURFACE

ON OPTIMIZATION OF TWO-TIER WALKER DELTA PATTERNS SATELLITE CONSTELLATIONS TO PROVIDE CONTINUOUS COVERAGE OF NEAR-EARTH SPACE SPHERICAL LAYER

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

DISTURBANCE OBSERVER-BASED FUZZY CONTROL FOR FLEXIBLE SPACECRAFT COMBINED ATTITUDE & SUN TRACKING SYSTEM

CONTROLLING THE MOTION OF A SPACECRAFT WHEN APPROACHING A LARGE OBJECT OF SPACE DEBRIS

SPACECRAFT THRUST VECTOR CONTROL DURING LANDING ON THE MOON SURFACE

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

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

METHOD OF TETHERED SYSTEM CONTROL FOR DEORBITING OBJECTS USING EARTH'S ATMOSPHERE

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

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

METHOD FOR CONSTELLATION DESIGN FOR EARTH PERIODIC COVERAGE USING COMPOUND SATELLITE STRUCTURES ON ORBITS WITH SYNCHRONIZED NODAL REGRESSION

FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 2: SYNTHESIS OF SATELLITE ORBITS AND CONSTELLATIONS

FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 4: COMPOUND SATELLITE STRUCTURES ON ORBITS WITH SYNCHRONIZED NODAL REGRESSION

EMULATING OF THE STATIONARY OBSERVATION OF THE EARTH LOCAL REGION USING LOCALLY GEOSTATIONARY ELLIPTIC ORBITS

FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 3: LOW-COST EARTH OBSERVATION WITH MINIMAL SATELLITE SWATH

METHOD OF OPTIMIZATION OF THE SERVICING SPACE-BASED SYSTEM ORBITS AND DETACHED UNITS MANEUVERES PARAMETERS IN THE PROBLEM OF ON-ORBIT-SERVICING OF THE GIVEN MULTI-SATELLITE SPACE INFRASTRUCTURE

FUNDAMENTALS OF THE ROUTE THEORY FOR SATELLITE CONSTELLATION DESIGN FOR EARTH DISCONTINUOUS COVERAGE. PART 1: ANALYTIC EMULATION OF THE EARTH COVERAGE

О ВНЕДРЕНИИ СОВРЕМЕННЫХ ТЕХНОЛОГИЙ УПРАВЛЕНИЯ ИННОВАЦИОННЫМИ ПРОЕКТАМИ

МНОГОКРИТЕРИАЛЬНЫЙ ПОДХОД К ЗАДАЧЕ ВЫБОРА ЭФФЕКТИВНОГО ИННОВАЦИОННОГО ПРОЕКТА

МОДЕЛЬ ОЦЕНКИ РИСКОВ В ПРОИЗВОДСТВЕ ВЫСОКОТЕХНОЛОГИЧНОЙ ПРОДУКЦИИ И ОЦЕНКА ИХ ВЛИЯНИЯ НА РОСТ СЕБЕСТОИМОСТИ И ЦЕНЫ

Other authors

Друшляков С.С.

Evtushenko O.N.