Astroinertial integrated navigation system 1Degtyarev AV, 2Makarov AL, 1Davydenko SA, 1Tykhonov VL, 3Laush AG. Astroinertial integrated navigation system. Kosm. nauka tehnol. 2016 ;22(2):29-37.
Voice barrier and influence of a powerful shock n-wave on resilient constructions of «air-to-air» type vehicles 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.
A method of trajectory processing for spacecrafts in multipositional optical complex 1Kovbasiuk SV, 1Kanevskyi LB. A method of trajectory processing for spacecrafts in multipositional optical complex. Kosm. nauka tehnol. 2012 ;18(3):38–45.
Some results of studies of the behaviour of a satellite in orbit in contingency mode under the near-Earth space influence 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.
On the motion of a microsatellite with the sail in the atmosphere (NanoSail-D) 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.
The thermal analysis of spacecrafts with orientation and geometric configuration varying during an orbit revolution. New software version 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.
Spacecraft control system’s reconfiguration in the presence of failures 1Melanchenko OG. Spacecraft control system’s reconfiguration in the presence of failures. Kosm. nauka tehnol. 2013 ;19(4):08–16.
Fault-tolerant control of Earth observation satellite with redundant configuration of reaction wheels 1Melanchenko OG. Fault-tolerant control of Earth observation satellite with redundant configuration of reaction wheels. Kosm. nauka tehnol. 2013 ;19(1):28–37.
The account of inaccuracy of satellite orientation in the course of shooting with nonzero angular velocity 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.
Achieving spacecraft rapid rotation using minimally redundant coplanar gyrodyne system 1Yefymenko MV, 2Lutsenko HV, 2Paromova TO. Achieving spacecraft rapid rotation using minimally redundant coplanar gyrodyne system. Kosm. nauka tehnol. 2015 ;21(5):48–56.