¹Shuvalov VA, ²Kochubey GS, ²Priymak AI, ²Pismenniy NI. High-altitude spacecraft power losses of solar arrays as a result of interaction with environment. Kosm. nauka tehnol. 2004 ;10(4):039-049.

¹Zlatkin Yu.M, ²Kalnoguz AN, ²Bataev VA, ²Kuzmin AI, ²Riumin MN, ²Yevtefeiev MP. The control of essentially non-symmetric runaway block with the engine working uninterruptedly. Kosm. nauka tehnol. 2004 ;10(4):032-038.

¹Kovbasiuk SV, ²Makhonin EI, ¹Pysarchuk ОО. The algorithm for the determination of spacecraft orbit parameters with the use of the Doppler gauge system. Kosm. nauka tehnol. 2004 ;10(4):027-031.

¹Shatikhin VE, ²Semenov LP, ³Artemenko YH, ⁴Borysenko VM, ³Helenko ОО. Oscillations caused by flexible attached elements of satellite constructions. Kosm. nauka tehnol. 2004 ;10(1):061-069.

¹Dranovsky VI, ²Zakrzhevskii AE, ³Khoroshylov VS. Dynamics of a deformed space system of bodies with programmed change of the configuration. Kosm. nauka tehnol. 2004 ;10(1):045-053.

¹Ischenko VI, ¹Zimchuk IV. A subsystem of the digital correction of control system of space vehicle orientation. Kosm. nauka tehnol. 2003 ;9(4):045-048.

¹Mel'nik VN, ¹Mahmut D, ¹Karachun VV, ¹Kunderevich EK. Errors of measurements of longitudinal speeds of rocket carriers by gyroscopic integrator. Kosm. nauka tehnol. 2002 ;8(1):081-088.

¹Aizenberg Ya.E, ¹Zlatkin Yu.M, ²Kalnoguz AN, ²Bataev VA, ²Kuzmin AI. Control on angles of attack and slip of the first stages of the launcher. Kosm. nauka tehnol. 2002 ;8(1):061-080.

¹Aizenberg Ya.E, ²Yastrebenetskii MA. Comparison of the safety principles for the control systems for launchers and atomic power stations. Kosm. nauka tehnol. 2002 ;8(1):055-060.

¹Mel'nik VN. About features speakers of a gyroscope with multiphase bracket in acoustics fields. Kosm. nauka tehnol. 2002 ;8(4):049-053.