¹Serdiuk OA, ¹Izhko VA, ¹Arzhannikov EV. Development of a high-speed software package for calculating the trajectory of launching a spacecraft into a geostationary orbit using the gravitational field of the moon with visualization of calculations. Kosm. nauka tehnol. 2004 ;10(Supplement1):059-062.

¹Yurchenko Yu.B. Reliability increment of onboard control complexes by means of lockstepped hardware voting majority frames construction at hardware synchronization of single-chip microcontrollers. Kosm. nauka tehnol. 2004 ;10(Supplement1):041-049.

¹Opachko II. On possibility of remote mass spectrometry analysis of space objects. Kosm. nauka tehnol. 2004 ;10(Supplement1):039-040.

¹Lysenko NA. Study of digital integrators in the detection of ultrasonic echo signals. Kosm. nauka tehnol. 2004 ;10(Supplement1):010-012.

¹Degtyarev AV, ¹Sheptun AD. Methodology, methods, and results of the first estimates of the probability of close approach between constellation satellites. Space Science and Technology. 2019 ;25(6):15-32.

¹Opachko II. On the possibility of space apparatus maneuvres under direct solar light conditions. Kosm. nauka tehnol. 2003 ;9(Supplement1):183-184.

¹Golubek AV, Yemel'yanova IA, Khorol'sk, ii PG. Investigation of the possibility of ballistic factor chage predicting on the basis of outer-trajectory measurements with the use of stable atmosphere parameters for calculations. Kosm. nauka tehnol. 2003 ;9(Supplement1):173-180.

Tsyruk AA, Yarovoi MA. Computer-aided design subsystem of primary structure of slender wing. Kosm. nauka tehnol. 2003 ;9(Supplement1):044-047.

Kuznetsov AV, ¹Larin VA, ¹Labutkina TV. Constructing non-conflict orbital satellite constellation. Kosm. nauka tehnol. 2003 ;9(Supplement1):033-036.

¹Tkachenko AI. Strengthened convergence of estimations in the in-flight geometric calibration. Space Science and Technology. 2019 ;25(4):41-47.