Fundamentals of the route theory for satellite constellation design for Earth discontinuous coverage. Part 1: Analytic emulation of the Earth coverage YN Razoumny Acta Astronautica 128, 722-740, 2016 | 50 | 2016 |
Disturbance observer-based fuzzy control for flexible spacecraft combined attitude & sun tracking system YC Chak, R Varatharajoo, Y Razoumny Acta Astronautica 133, 302-310, 2017 | 40 | 2017 |
Large-size space debris flyby in low Earth orbits AA Baranov, DA Grishko, YN Razoumny Cosmic Research 55, 361-370, 2017 | 27 | 2017 |
Flyby of large-size space debris objects and their transition to the disposal orbits in LEO AA Baranov, DA Grishko, YN Razoumny, L Jun Advances in Space Research 59 (12), 3011-3022, 2017 | 27 | 2017 |
Fundamentals of the route theory for satellite constellation design for Earth discontinuous coverage. Part 2: Synthesis of satellite orbits and constellations YN Razoumny Acta Astronautica 128, 741-758, 2016 | 24 | 2016 |
Route satellite constellations for earth discontinuous coverage and optimal solution peculiarities YN Razoumny Journal of Spacecraft and Rockets 54 (3), 572-581, 2017 | 18 | 2017 |
Fundamentals of the route theory for satellite constellation design for Earth discontinuous coverage. Part 3: Low-cost Earth observation with minimal satellite swath YN Razoumny Acta Astronautica 129, 447-458, 2016 | 18 | 2016 |
Fundamentals of the route theory for satellite constellation design for Earth discontinuous coverage. Part 4: Compound satellite structures on orbits with synchronized nodal … YN Razoumny Acta Astronautica 129, 459-465, 2016 | 15 | 2016 |
New research methodology for Earth periodic coverage and regularities in parametric localization of optimal low-Earth-orbit satellite constellations YN Razoumny Adv. Astronaut. Sci 150, 3117-3136, 2014 | 15 | 2014 |
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 … Y Razoumny, V Razoumny, P Kozlov, A Baranov, R Varatharajoo Proceedings of the International Astronautical Congress, IAC, 2016 | 12 | 2016 |
Spacecraft guidance, navigation and control based on application of resonant tunneling diodes in nonlinear radio signal converters MO Makeev, SA Meshkov, VY Sinyakin, YN Razoumny Advances in the Astronautical Sciences, 475-482, 2017 | 10 | 2017 |
Analytic solutions for Earth discontinuous coverage and methods for analysis and synthesis of satellite orbits and constellations YN Razoumny AIAA/AAS Astrodynamics Specialist Conference, 4160, 2014 | 9 | 2014 |
The concept of On-Orbit-Servicing for next generation space system development and its key technologies YN Razoumny, DB Spencer, B Agrawal, J Kreisel, T Yasaka, ... 68th International Astronautical Congress: Unlocking Imagination, Fostering …, 2017 | 8 | 2017 |
Principle of motion based on the kinetic moment DB Spencer, YN Razoumny, SA Kupreev Advances in the Astronautical Sciences 174, 301-307, 2021 | 6 | 2021 |
On optimization of Earth coverage characteristics for compound satellite constellations based on orbits with synchronized nodal regression YN Razoumny, PG Kozlov, VY Razoumny, AA Moshnin Proceedings of the 2nd IAA Conference on Dynamics and Control of Space Systems, 2014 | 6 | 2014 |
Optimization of Designed Ballistic Parameters of Satellite Systems for the Earth Periodical Coverage YN Razoumny Earth Research from Space 14 (1), 48-58, 1993 | 6 | 1993 |
Method of Parameters Optimization of the One-Route Earth Artificial Satellite Systems for the Earth Periodical Coverage YN Razoumny Earth Research from Space, 39-46, 1991 | 6 | 1991 |
The research method of controlled movement dynamics of tether system YN Razoumny, SA Kupreev, AK Misra Advances in the Astronautical Sciences 170, 417-431, 2020 | 5 | 2020 |
Low orbit spacecraft service planning AA Baranov, VY Razoumny, YN Razoumny, VV Malyshev Proceedings of the International Astronautical Congress, IAC68, 835-844, 2017 | 5 | 2017 |
Method for satellite orbit and constellation design for Earth discontinuous coverage with minimal satellite Swath under the given constraint on the maximum revisit time YN Razoumny Advances in the Astronautical Sciences Spaceflight Mechanics 2015 155, 2337-2356, 2015 | 5 | 2015 |