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Spacecraft Dynamics and Control

Mutual relations of internal coordinate systems of star sensors in the problem of accurate determination of spacecraft orientation

¹Efimenko NV. Mutual relations of internal coordinate systems of star sensors in the problem of accurate determination of spacecraft orientation. Kosm. nauka tehnol. 2013 ;19(6):12-17.

Iintellectual control system for spacecraft rendezvous and docking based on active optical markers and its laboratory prototyping

¹Taranenko VB, ¹Lymarenko RA, ¹Topolnikov VA, ²Yatsenko VA, ³Martysh EV, ⁴Melanchenko OG. Iintellectual control system for spacecraft rendezvous and docking based on active optical markers and its laboratory prototyping. Kosm. nauka tehnol. 2015 ;21(2):53–55.

Numerical modelling of supersonic flow around a wedge with the use of free open software code OpenFOAM

¹Karvatskii AYa., ¹Pulinets IV, ¹Lazarev ТВ, ¹Pedchenko AYu. Numerical modelling of supersonic flow around a wedge with the use of free open software code OpenFOAM. Kosm. nauka tehnol. 2015 ;21(2):47–52.

Determination of orientation, coordinates, relative position and movement parameters of objects in space with the GNSS technology

¹Lutsenko IV, ¹Popov DO, ²Laush AG, ³Yatsenko VO, ⁴Zhalilo OO, ⁵Ditskiy IV, ⁶Bessonov EA. Determination of orientation, coordinates, relative position and movement parameters of objects in space with the GNSS technology. Kosm. nauka tehnol. 2015 ;21(2):40–46.

Research of dynamic regularities of electrodynamic space tethered system as a possible highly efficient passive deorbit systems for space debris at the low earth orbits

¹Maslova AI, ²Mischenko AV, ¹Pirozhenko AV, ²Khramov DA. Research of dynamic regularities of electrodynamic space tethered system as a possible highly efficient passive deorbit systems for space debris at the low earth orbits. Kosm. nauka tehnol. 2015 ;21(1):20–24.

The estimate of dynamic response of spacecraft and launcher fragmentation system components under impulsive loading

¹Shulzhenko MG, ²Zajtsev BP, ¹Gontarovskyi PP, ²Protasova TV, ³Batutina TYa., ⁴Sheremet IV. The estimate of dynamic response of spacecraft and launcher fragmentation system components under impulsive loading. Kosm. nauka tehnol. 2015 ;21(1):15–19.

Dynamic instability of rockets fairings

¹Avramov KV, ¹Chernobryvko MV, ²Batutina TYa., ³Degtyarenko PG, ²Tonkonozhenko AM. Dynamic instability of rockets fairings. Kosm. nauka tehnol. 2015 ;21(1):10–14.

Development of robust methods of precision attitude control of small spacecrafts and their implementation at the problem-oriented processors

¹Kuntsevich VM, ²Palagin OV, ³Gubarev VF, ⁴Babii NА, ³Volosov VV, ²Lisovyi OM, ³Melnychuk SV, ²Opanasenko VM, ³Shevchenko VM. Development of robust methods of precision attitude control of small spacecrafts and their implementation at the problem-oriented processors. Kosm. nauka tehnol. 2015 ;21(1):03–09.

Coincidence resonancein hypersound flight conditions

¹Boiko GV. Coincidence resonancein hypersound flight conditions. Kosm. nauka tehnol. 2014 ;20(3):28-33.

Determining spacecraft orientation using information from two jointly processed star trackers

¹Efimenko NV. Determining spacecraft orientation using information from two jointly processed star trackers. Kosm. nauka tehnol. 2014 ;20(3):22-27.

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