Selecting the conditions of nanosatellite separation from the upper stage of the arrier-rocket "Soyuz" in undirected flight
Avaryaskin D.P., Belokonov I.V., Timbay I.A., Lagno O.G.
Simulation of the process of angular rate damping of the SamSat-218D nanosatellite after separation from the launching-transporting container
Melnik M.E.
Relative equilibria of dynamically symmetric CubeSat nanosatellite under the action of aerodynamic and gravitational torques
Barinova E.V., Timbai I.A.
Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy
Sinitsin L.I., Belokonov I.V.
Analysis of SamSat-218D nanosatelite motion acording to trajectory measurements
Belokonov I.V., Timbai I.A., Nikolaev P.N., Orazbaeva U.M.
Selection of project structure for nanosatellite propulsion system
Belokonov I.V., Ivliev A.V., Bogatyrev A.M., Kumarin A.A., Lomaka I.A., Simakov S.P.
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.
On-board algorithm for SamSat-218D nanosatellite orientation and stabilization system
Kramlikh A.V., Melnik M.E.
Possibility of using leo satellite communication systems for on-line data interchange
Davydov D.D.
Determination of relative position and orientation of nanosatellites by video image analysis
Simakov S.P., Ustyugov E.V.
Mathematical model of angular motion of nanosatellites with inertial actuators
Moldabekov M.M., Ahmedov D.S., Elubaev S.A., Sukhenko A.S., Bopeev T.M., Alipbayev K.A., Mikhailenko D.L.
Determination of the maximum values of the spatial angle of attack of a nanosatellite in motion on lowcircular orbits
Glukhova L.V., Timbai I.A.
Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation
Tsaplin S.V., Bolychev S.A.
Optimal control laws of onboard coils for the reduction of angular momentum and damping of angular velocity of nanosatellites and microsatellites with magnetic coils on board
Lyubimov V.V., Podkletnova S.V.
Three-dimensional inhomogeneous thermal fields of the “Photon-Amur 2.0” payload electronic board developed for nanosatellites
Fomin D.V., Barulinа M.A., Golikov A.V., Strukov D.O., German A.S., Ogorodnikov A.A.
Selection of a nanosatellite group separation program for cluster launching from the «Soyuz» launch vehicle orbiter
Avaryaskin D.P., Shcherbakov M.S.
1 - 16 of 16 Items

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