Author Details

Белоконов, И. В.

Issue	Section	Title	File
Vol 12, No 4 (2013)	ISSUE WITHOUT SECTION	Selecting the conditions of nanosatellite separation from the upper stage of the arrier-rocket "Soyuz" in undirected flight	(Rus)
Vol 12, No 4 (2013)	ISSUE WITHOUT SECTION	Analysis of the influence of low-orbit nanosatellite uncontrolled motion on the possibility of solving navigation and communication problems after its separation from the «Soyuz» carrier rocket upper-stage	(Rus)
Vol 6, No 1 (2007)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Space vehicle attitude control recovery procedure combining magnetometric and padionavigation measurements	(Rus)
Vol 3, No 1 (2004)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Estimation of efficiency of controlling scientific experiments at autonomous microgravitational space platforms	(Rus)
Vol 5, No 1 (2006)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Problems of relational navigation in load transporation on helicopter external hanger	(Rus)
Vol 6, No 1 (2007)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Modelling the interaction of micrometeoroid and technogenous particles with a space vehicle	(Rus)
Vol 9, No 2 (2010): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent	(Rus)
Vol 11, No 4 (2012)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Analysis of uncontrolled motion of the “ Soyuz “ carrier rocket orbital stage after payload separation	(Rus)
Vol 1, No 1 (2002)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Dynamics and motion control of aerospace and space-rocket systems	(Rus)
Vol 18, No 2 (2019)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Determining the dynamics of spacecraft rotational motion with the use of information provided by global navigation satellite systems	(Rus)
Vol 18, No 3 (2019)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Selection of project structure for nanosatellite propulsion system	(Rus)
Vol 18, No 4 (2019)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Analysis of SamSat-218D nanosatelite motion acording to trajectory measurements	(Rus)
Vol 20, No 1 (2021)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy	(Rus)

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