¹Krivonosov AI, ¹Kulakov AA, ¹Baida NK, ²Kharchenko VS, ³Blagodarny NP. Structure algorithm organization and reliability models of reserved systems. Kosm. nauka tehnol. 1995 ;1(1):74–79.

¹Aizenberg Ya.E. Concept of developing the control system for automatic spacecraft of "Spectrum" series. Kosm. nauka tehnol. 1995 ;1(1):35–46.

¹Kalynychenko DS, ²Baranov Ye.Yu., ²Poluian MV. Effiecency criterion for selection of design parameters of aerospace system. Kosm. nauka tehnol. 2016 ;22(2):48-51.

¹Ivanova VI, ¹Sheptun AD. Ensuring maximum stability of Earth remote sensing conditions without the orbit correction. Kosm. nauka tehnol. 2016 ;22(2):38-47.

¹Degtyarev AV, ²Makarov AL, ¹Davydenko SA, ¹Tykhonov VL, ³Laush AG. Astroinertial integrated navigation system. Kosm. nauka tehnol. 2016 ;22(2):29-37.

¹Mel’nick VN, ¹Karachun VV. Voice barrier and influence of a powerful shock n-wave on resilient constructions of «air-to-air» type vehicles. Kosm. nauka tehnol. 2012 ;18(5):12–23.

¹Kovbasiuk SV, ¹Kanevskyi LB. A method of trajectory processing for spacecrafts in multipositional optical complex. Kosm. nauka tehnol. 2012 ;18(3):38–45.

¹Epishev VP, ¹Isak II, ¹Kudak VI, ¹Motrunich II, ¹Noibauer IF, ²Koshkin NI, ³Bilinsky AI, ³Martyniuk-Lototskij KP, ⁴Blagodyr Ya.T, ⁵Lopachenko VV, et al. Some results of studies of the behaviour of a satellite in orbit in contingency mode under the near-Earth space influence. Kosm. nauka tehnol. 2012 ;18(1):60–67.

¹Koshkin NI, ²Korobeynikova EA, ³Lopachenko VV, ²Melikyants SM, ²Strakhova SL, ²Shakun LS. On the motion of a microsatellite with the sail in the atmosphere (NanoSail-D). Kosm. nauka tehnol. 2012 ;18(1):31–38.

¹Kislov AM, ¹Romanenko VG, ¹Fenchenko VN. The thermal analysis of spacecrafts with orientation and geometric configuration varying during an orbit revolution. New software version. Kosm. nauka tehnol. 2012 ;18(1):21–30.