Spacecraft control system’s reconfiguration in the presence of failures
. Spacecraft control system’s reconfiguration in the presence of failures. Kosm. nauka tehnol. 2013 ;19(4):08–16.
Spacecraft Dynamics and Control
Fault-tolerant control of Earth observation satellite with redundant configuration of reaction wheels
. 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
. 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
. Achieving spacecraft rapid rotation using minimally redundant coplanar gyrodyne system. Kosm. nauka tehnol. 2015 ;21(5):48–56.
Mutual relations of internal coordinate systems of star sensors in the problem of accurate determination of spacecraft orientation
. Mutual relations of internal coordinate systems of star sensors in the problem of accurate determination of spacecraft orientation. Kosm. nauka tehnol. 2013 ;19(6):12-17.
Iintellectual control system for spacecraft rendezvous and docking based on active optical markers and its laboratory prototyping
. Iintellectual control system for spacecraft rendezvous and docking based on active optical markers and its laboratory prototyping. Kosm. nauka tehnol. 2015 ;21(2):53–55.
Numerical modelling of supersonic flow around a wedge with the use of free open software code OpenFOAM
Numerical modelling of supersonic flow around a wedge with the use of free open software code OpenFOAM. Kosm. nauka tehnol. 2015 ;21(2):47–52.
Determination of orientation, coordinates, relative position and movement parameters of objects in space with the GNSS technology
. Determination of orientation, coordinates, relative position and movement parameters of objects in space with the GNSS technology. Kosm. nauka tehnol. 2015 ;21(2):40–46.
Research of dynamic regularities of electrodynamic space tethered system as a possible highly efficient passive deorbit systems for space debris at the low earth orbits
. Research of dynamic regularities of electrodynamic space tethered system as a possible highly efficient passive deorbit systems for space debris at the low earth orbits. Kosm. nauka tehnol. 2015 ;21(1):20–24.
The estimate of dynamic response of spacecraft and launcher fragmentation system components under impulsive loading
. The estimate of dynamic response of spacecraft and launcher fragmentation system components under impulsive loading. Kosm. nauka tehnol. 2015 ;21(1):15–19.