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Publications in Math-Net.Ru
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About finding new methods and forms of solving the Euler–Lambert equation
Program Systems: Theory and Applications, 9:4 (2018), 293–305
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About the influence of spacecraft maneuverability characteristics on the convergence objects observing possibility
Program Systems: Theory and Applications, 5:2 (2014), 19–31
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About the control and correction of exoatmospheric orbit-descent trajectory area for planet artificial satellite
Program Systems: Theory and Applications, 5:2 (2014), 13–18
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The repositioning maneuver of artificial Earth satellite in a circular orbit with a supporting acceleration
Program Systems: Theory and Applications, 4:4 (2013), 3–15
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The repositioning maneuver of artificial Earth satellite in a circular orbit with the phasing coils trajectory
Program Systems: Theory and Applications, 4:1 (2013), 3–14
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Hodographs and the equation of flight in a central gravitational field
Program Systems: Theory and Applications, 3:3 (2012), 81–95
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The repositioning maneuver of artificial Earth satellite in a circular orbit with the phasing coils trajectory
Program Systems: Theory and Applications, 3:3 (2012), 71–79
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