Spacecraft Dynamics and Control

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.

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.

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.

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