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Title
Authors
Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy
Sinitsin L.I., Belokonov I.V.
Possibility of using leo satellite communication systems for on-line data interchange
Davydov D.D.
Analysis of SamSat-218D nanosatelite motion acording to trajectory measurements
Belokonov I.V., Timbai I.A., Nikolaev P.N., Orazbaeva U.M.
Determination of relative position and orientation of nanosatellites by video image analysis
Simakov S.P., Ustyugov E.V.
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.
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.
Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation
Tsaplin S.V., Bolychev S.A.
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.
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.
Biological module “BiNOM” for cubesats of the SamSat family
Zakharov V.P., Konyukhov V.N., Bakhtinov P.I., Molchkov E.V., Kornilin D.V., Konovalov S.G.
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.
Procedure of assessing the error of the device for measuring mass-centering and inertial characteristics of nanosatellites using reference objects
Vasin P.V., Barinova E.V.
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.
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.
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.
On-board algorithm for SamSat-218D nanosatellite orientation and stabilization system
Kramlikh A.V., Melnik M.E.
1 - 17 of 17 Items

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