Bypass maneuver by radial boosting impulse 1Avdeev VV, 2Khorolskyi PG. Bypass maneuver by radial boosting impulse. Kosm. nauka tehnol. 2002 ;8(4):043-048.
Singular optimal controls in the mechanics of space flight 1Kiforenko BN. Singular optimal controls in the mechanics of space flight. Kosm. nauka tehnol. 2017 ;23(3):82-84.
Manoeuvre to bypass a dangerous zone by a satellite with thruster of low tractive force and radial direction 1Avdeev VV. Manoeuvre to bypass a dangerous zone by a satellite with thruster of low tractive force and radial direction. Kosm. nauka tehnol. 2007 ;13(3):027-030.
Effects of magnetohydrodynamic control in heat exchange and decelaration of magnetized bodies in the earth's atmosphere and magnetosphere 1Shuvalov VA, 2Priymak AI, 2Bandel KA, 2Kochubey GS, 1Tokmak NA. Effects of magnetohydrodynamic control in heat exchange and decelaration of magnetized bodies in the earth's atmosphere and magnetosphere. Kosm. nauka tehnol. 2008 ;14(4):27-38.
Qualification tests of the critical software for space systems: target technology of independent verification and latent defect prediction 1Konorev BM, 2Alekseev Yu.G, 3Zasuha SA, 3Semenov LP, 4Kharchenko VS, 2Chertkov GN. Qualification tests of the critical software for space systems: target technology of independent verification and latent defect prediction. Kosm. nauka tehnol. 2008 ;14(4):09-26.
Management of oscillatory contour of micromechanical system 1Zbruts'kyi OV, 1Havrylenko VV, 1Stetsenko TV. Management of oscillatory contour of micromechanical system. Kosm. nauka tehnol. 2009 ;15(1):71-74.
Atmosphere density changes caused by the motion of spacecrafts in low Earth orbits 1Maslova AI, 1Pirozhenko AV. Atmosphere density changes caused by the motion of spacecrafts in low Earth orbits. Kosm. nauka tehnol. 2009 ;15(1):13-18.
Orbit height increase by low thrust in transversal direction 1Avdeev VV. Orbit height increase by low thrust in transversal direction. Kosm. nauka tehnol. 2009 ;15(1):09-12.
Strapdown initial exhibition of rockets with inclined start 1Kalnoguz AN, 1Tykhovskiy VM, 1Bataev VA, 1Ryumin MN, 1Pilguy VN. Strapdown initial exhibition of rockets with inclined start. Kosm. nauka tehnol. 2010 ;16(4):37-45.
COMBINATORIC METHOD FOR INTERVAL ESTIMATION OF A SPACECRAFT ATTITUDE BASED ON STAR TRACKER MEASUREMENTS 1Gubarev VF, 2Melnychuk SV. COMBINATORIC METHOD FOR INTERVAL ESTIMATION OF A SPACECRAFT ATTITUDE BASED ON STAR TRACKER MEASUREMENTS. Kosm. nauka tehnol. 2016 ;22(6):10-19.