¹Ermolenko EA, ¹Kamenchuk Yu.V. Method of determination of aerodynamic axial force acting on vehicle body and stabilizer on it. Kosm. nauka tehnol. 2001 ;7(Supplement1):089-092.

¹Andronov VA, ¹Novikov AV. Controllability ensuring during stages separation of launch vechicle low controller effectiveness of second stage. Kosm. nauka tehnol. 2001 ;7(Supplement1):082-088.

¹Zuyev AL. On partial stabilization of satellite orientation by means of two control torques. Kosm. nauka tehnol. 2001 ;7(Supplement1):076-081.

¹Ivanova VI, ²Ivanov OM. Orbital motion project for Globalstar-system spacecraft group launch. Kosm. nauka tehnol. 2001 ;7(Supplement1):074-076.

¹Koshevoi OV. Preliminary specification of spacecraft orbital elements by moment of separation based on one measurement session. Kosm. nauka tehnol. 2001 ;7(Supplement1):072-073.

¹Ivanov OM, ¹Mashtak IV, ¹Shkarupin VV. Ballistic-navigational support of Sich-1 flight, the first Ukrainian satellite. results and attainments. Kosm. nauka tehnol. 2001 ;7(Supplement1):068-072.

¹Belousov KG, ²Melanchenko OG. Definition of disturbing moment effecting on satellite in flight by telemetry data. Kosm. nauka tehnol. 2001 ;7(Supplement1):067-068.

¹Safronov AV, ²Semon BY, ¹Nedilko AN. Flexural-torsional flutter of an aerrodynamic profile with irregular compaction. Space Science and Technology. 2019 ;25(2):12-21.

¹Pirozhenko AV, ¹Maslova AI, ²Vasilyev VV. About the influence of second zonal harmonic on the motion of satellite in almost circular orbits. Space Science and Technology. 2019 ;25(2):03-11.

¹Yefymenko MV. Explicit laws for tuning power gyroscopic complexes of multiple circuits in problems of controlling the orientation of a spacecraft. Space Science and Technology. 2019 ;25(1):27-37.