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Vol 20, No 1 (2021)

Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy

Sinitsin L.I., Belokonov I.V.

(Rus)

Vol 15, No 1 (2016)

Possibility of using leo satellite communication systems for on-line data interchange

Davydov D.D.

(Rus)

Vol 18, No 4 (2019)

Analysis of SamSat-218D nanosatelite motion acording to trajectory measurements

Belokonov I.V., Timbai I.A., Nikolaev P.N., Orazbaeva U.M.

(Rus)

Vol 15, No 1 (2016)

Determination of relative position and orientation of nanosatellites by video image analysis

Simakov S.P., Ustyugov E.V.

(Rus)

Vol 18, No 3 (2019)

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.

(Rus)

Vol 15, No 1 (2016)

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.

(Rus)

Vol 18, No 2 (2019)

Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation

Tsaplin S.V., Bolychev S.A.

(Rus)

Vol 15, No 1 (2016)

Simulation of the process of angular rate damping of the SamSat-218D nanosatellite after separation from the launching-transporting container

Melnik M.E.

(Rus)

Vol 18, No 2 (2019)

Relative equilibria of dynamically symmetric CubeSat nanosatellite under the action of aerodynamic and gravitational torques

Barinova E.V., Timbai I.A.

(Rus)

Vol 12, No 4 (2013)

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.

(Rus)

Vol 17, No 2 (2018)

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.

(Rus)

Vol 12, No 4 (2013)

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.

(Rus)

Vol 21, No 3 (2022)

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.

(Rus)

Vol 15, No 2 (2016)

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.

(Rus)

Vol 12, No 4 (2013)

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.

(Rus)

Vol 20, No 2 (2021)

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.

(Rus)

Vol 15, No 2 (2016)

On-board algorithm for SamSat-218D nanosatellite orientation and stabilization system

Kramlikh A.V., Melnik M.E.

(Rus)

1 - 17 of 17 Items

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