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. Control on angles of attack and slip of the first stages of the launcher. Kosm. nauka tehnol. 2002 ;8(1):061-080.
. Comparison of the safety principles for the control systems for launchers and atomic power stations. Kosm. nauka tehnol. 2002 ;8(1):055-060.
. High accuracy stabilization system of launch vehicle with asymmetric configuration when one engine failure is possible. Kosm. nauka tehnol. 1998 ;4(1):64–67.
. Dynamic testing of on-board embedded computer software of missile and spacecraft control system. Kosm. nauka tehnol. 1997 ;3(1):61–74.
. Efficient algorithms for space image processing and their realization in cellular neural networks. Kosm. nauka tehnol. 1998 ;4(4):74–84.
. Concept of developing the control system for automatic spacecraft of "Spectrum" series. Kosm. nauka tehnol. 1995 ;1(1):35–46.
. Physical foundation for the construction of paraffin-based hybrid rocket engines. Кinetics of melting and combustion. Kosm. nauka tehnol. 2011 ;17(3):28-33.
. Perturbed motion of the artificial satellite of the Moon in the project «UkrSelena». Kosm. nauka tehnol. 2009 ;15(1):05-08.
. Prospects of the rocket-space branch of Ukraine is the rocket system on the basis of the airborne-spase vehicle. Kosm. nauka tehnol. 2006 ;12(4):003-013.