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Relative equilibria of dynamically symmetric CubeSat nanosatellite under the action of aerodynamic and gravitational torques
Barinova E.V., Timbai I.A.
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
Belokonov I.V., Kramlikh A.V., Timbai I.A.
Analysis of uncontrolled motion of the “ Soyuz “ carrier rocket orbital stage after payload separation
Belokonov I.V., Storozh A.D., Timbai I.A.
Research of planar motion of spacecraft around its center of mass under the influence of the gravitational and the aerodynamic moments during its descent from circular orbits
Glukhova L.V., Timbay I.A.
Deviation of reentry spacecraft from the estimated trajectory caused by transient modes of angular motion at the stage of entry into the atmosphere
Barinova Y.V., Timbay I.A.
Research of spatial motion of an uncontrolled spacecraft with the triharmonic moment characteristics around its center of mass during its reentry into atmosphere
Barinova Y.V., Timbay I.A.
Analysis of plane motion relative to the centre of mass of a descent capsule with the three-harmonic moment characteristics during its reentry
1 1., 1 1.
Research of small spacecraft dynamiсs taking into account the influence of elastic vibrations of asjacent solar panels and aerodynamic moment
Yelenev V.D., Titov B.A., Davydov E.I., Davydov I.E., Kochyan A.G., Yudintsev V.V.
1 - 8 of 8 Items

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