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.

¹Melanchenko OG. Spacecraft control system’s reconfiguration in the presence of failures. Kosm. nauka tehnol. 2013 ;19(4):08–16.

¹Melanchenko OG. Fault-tolerant control of Earth observation satellite with redundant configuration of reaction wheels. Kosm. nauka tehnol. 2013 ;19(1):28–37.

¹Makarov AL, ²Mozgovoy DK, ³Kulabukhov AM, ¹Khoroshylov VS, ¹Balashov VN, ¹Popel' VM. The account of inaccuracy of satellite orientation in the course of shooting with nonzero angular velocity. Kosm. nauka tehnol. 2013 ;19(1):20–27.

¹Yefymenko MV, ²Lutsenko HV, ²Paromova TO. Achieving spacecraft rapid rotation using minimally redundant coplanar gyrodyne system. Kosm. nauka tehnol. 2015 ;21(5):48–56.

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.