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Vol 23, No 4 (2024)

Methodology of calculating on-board equipment arranging coordinates with preliminary estimate of on-board cable system mass

Belyakov A.A., Shulepov A.I., Papazov V.М., Prihodko V.I., Fedosov A.V.

(Rus)

Vol 22, No 2 (2023)

Simulating the process of retargeting of optoelectronic Earth observation spacecraft during object shooting

Kurenkov V.I., Pupkov E.A., Kucherov A.S.

(Rus)

Vol 22, No 3 (2023)

Models for determining the orientation of the solar battery of an observation spacecraft relative to the Sun during object survey and retargeting

Kurenkov V.I., Pupkov E.A.

(Rus)

Vol 22, No 3 (2023)

Classification and comparative analysis of methods for limiting technogenic pollution in the near-Earth space

Klyushnikov V.Y., Zakharova A.P., Usovik I.V.

(Rus)

Vol 22, No 3 (2023)

Digital model of the drag force of the Earth’s upper atmosphere for the design of low-orbit spacecraft

Volotsuev V.V.

(Rus)

Vol 23, No 3 (2024)

Estimating the design parameters of a space-based radio surveillance system

Ivanushkin M.A., Zhaldybina O.D., Safronov S.L., Korovin M.D.

(Rus)

Vol 21, No 4 (2022)

Basic aspects of topological technology of automated on-board equipment layout in space vehicle compartments using the example of “Yantar-2k” Earth remote sensing space vehicle

Belyakov A.A., Shulepov A.I.

(Rus)

Vol 17, No 4 (2018)

Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft

Ryzhkov V.V., Sulinov A.V.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

Automated generation of structural members of a spacecraft thermal model

Kulikov D.S., Shatin A.A., Velmisov I.G.

(Rus)

Vol 23, No 1 (2024)

Analysis and improvement of characteristics of power supply systems for the small space vehicle of the AIST-2 type

Mordanov M.R., Safronov S.L.

(Rus)

Vol 23, No 1 (2024)

Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface

Kovalev V.V., Marchenko A.D., Starostina T.V., Sharipova A.R.

(Rus)

Vol 21, No 1 (2022)

Isotopy of spacecraft compartment hull shapes

Belyakov A.A., Shulepov A.I.

(Rus)

Vol 22, No 4 (2023)

Features of the use of directional fixed antennas of a high-speed radio link on a small spacecraft AIST-2T

Eremina V.V., Erkov I.O., Zhuravlev A.A., Maslov I.V., Pyrinov N.I.

(Rus)

Vol 15, No 2 (2016)

Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem

Tsaplin S.V., Bolychev S.A.

(Rus)

Vol 23, No 4 (2024)

Method of testing the software of spacecraft electronic equipment based on fault injection in the algorithms of orientation and stabilization

Nedorezov D.A., Postnikov A.I., Murigin A.V., Shnaider A.V.

(Rus)

Vol 23, No 4 (2024)

Simulation of the onboard energy balance of spacecraft for Earth remote sensing

Kurenkov V.I., Pupkov E.A., Tkachenko I.S.

(Rus)

Vol 18, No 4 (2019)

Optimal control of spacecraft motion in the vicinity of Eros 433 asteroid

Shornikov A.Y.

(Rus)

Vol 16, No 3 (2017)

Modeling external thermal influence of infrared radiation sources during tests of rocket and space equipment in VK-600/300

Dobritsa D.B., Ushakova A.A., Shabarchin A.F., Yashchenko B.Y.

(Rus)

Vol 15, No 1 (2016)

Small spacecraft for the registration of micrometeorites and space debris

Semkin N.D., Telegin А.М., Vidmanov A.S.

(Rus)

Vol 14, No 2 (2015)

Computational algorithm of forming program motion in a scheduled turn of small spacecraft

Salmin V.V., Filatov A.V., Tkachenko I.S., Tyugashev A.A., Sopchenko E.V.

(Rus)

Vol 13, No 4 (2014)

Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine

Ishkov S.A., Filippov G.A.

(Rus)

Vol 9, No 2 (2010): Special Issue

Methods of measurement and calculation of microaccelerations onboard of low orbit space microgravitational platform

1 1., 1 1., 1 1.

(Rus)

Vol 12, No 1 (2013)

Improvements in methods of analysis and control of space-rocket equipment reliability at the stage of complex electrical testing

Belova V.V.

(Rus)

Vol 21, No 1 (2022)

Influence of space vehicle remote power supply on thermal regimes of solar batteries

Steganov G.B., Beznyakov A.M., Nemirov A.V.

(Rus)

Vol 18, No 4 (2019)

Control program for noncoplanar heliocentric flight to Venus of non-perfectly reflecting solar sail spacecraft

Khabibullin R.M.

(Rus)

Vol 17, No 2 (2018)

Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft

Igolkin A.A., Safin A.I., Filipov A.G.

(Rus)

Vol 15, No 3 (2016)

Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft

Semkin N.D., Piyakov I.V., Rodina M.A., Rodin D.V.

(Rus)

Vol 15, No 1 (2016)

Results of operation of scientific hardware «Space system of microacceleration compensation»

Semkin N.D., Piyakov I.V.

(Rus)

Vol 14, No 1 (2015)

Concept of multilevel adaptation of integrated navigation systems of small spacecraft

Fominov I.V.

(Rus)

Vol 11, No 5-2 (2012): Special Issue

Synthesis of dynamic modes of attitude motion of spacecraft with solid propellant rocket engine

Balakin V.L., Doroshin A.V., Krikunov M.M.

(Rus)

Vol 13, No 1 (2014)

Sensor equipment “Shtil-M” for carrying out experiments on the “Resource-P” spacecraft

Semkin N.D., Voronov K.E., Pomelnikov R.A., Shatrov S.A., Piyakov A.V., Bragin V.V.

(Rus)

Vol 9, No 2 (2010): Special Issue

The rotation maneuvers and synthesis of gyromoment guidance laws for land-survey spacecraft

1 1., 1 1., 1 1.

(Rus)

Vol 12, No 2 (2013)

Method of calculating self-capacitance in planar structural elements of a spacecraft

Syomkin N.D., Bragin V.V., Pomelnikov R.A., Balakin V.L.

(Rus)

Vol 18, No 4 (2019)

Comparative estimation of the accuracy of methods of autonomous navigation of small spacecraft in formation flying

Golyakov A.D., Richnyak A.M., Kalabin P.V.

(Rus)

Vol 17, No 2 (2018)

Accuracy of autonomous navigation by the mutual method in the case of a group flight of space vehicles

Golyakov A.D., Richnyak A.M.

(Rus)

Vol 15, No 3 (2016)

Spacecraft power supply system using additional low-power sources of energy

Kargu D.L., Beznyakov A.M., Nemirov A.V.

(Rus)

Vol 15, No 1 (2016)

Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit

Ishkov S.A.

(Rus)

Vol 14, No 1 (2015)

Device for monitoring radiation situation on spacecraft

Syomkin N.D., Plokhotnichenko P.G., Ilyin A.B., Kalaev M.P., Ryazanov D.M., Pomel'nikov P.A.

(Rus)

Vol 11, No 4 (2012)

Method of choosing spacecraft design characteristics on the basis of creating task-oriented systems of computer-aided design

Kucherov A.S., Kurenkov V.I.

(Rus)

Vol 13, No 1 (2014)

Problems of unmanned spacecraft reengineering in abnormal flight situations and their knowledge-based solutions

Akhmetov R.N., Makarov V.P., Sollogub A.V.

(Rus)

Vol 9, No 1 (2010)

Choosing the structure of power-supply systems for low-orbit space vehicles

1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 12, No 4 (2013)

Influence of the reliability of Earth remote sensing spacecraft onboard systems on the monitoring of imaging periodicity

Kirilin A.N., Akhmetov R.N., Kurenkov V.I., Kapitonov V.A., Stratilatov N.R., Lokhmatkin V.V.

(Rus)

Vol 20, No 3 (2021)

Estimation and analysis of the influence of ionizing radiation on the operation of nanosatellite onboard radio electronic equipment

Tsaplin S.V., Bolychev S.A.

(Rus)

Vol 18, No 2 (2019)

Reduction of angular velocities of AIST-2D spacecraft using a system of kinetic moment dumping

Shipov M.G.

(Rus)

Vol 17, No 1 (2018)

Determination of spacecraft antenna directivity pattern with the use of an Earth-based station

Vasyutkina O.V., Vopilin A.V., Raduchev S.V., Khalilov R.R., Yakunin V.S.

(Rus)

Vol 15, No 1 (2016)

Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system

Zabolotnov Y.M., Lobankov A.A.

(Rus)

Vol 14, No 1 (2015)

Electrization of the surface of low-orbiting small spacecraft “AIST”

Syomkin N.D., Bragin V.V., Piyakov A.V., Telegin A.M., Ryazanov D.M., Matviets M.G.

(Rus)

Vol 11, No 4 (2012)

Adaptive algorithm of determining low altitude spacecraft orientation on the basis of processing instant diverse-type measurements

Grigoryeva M.Y., Kramlikh A.V.

(Rus)

Vol 10, No 2 (2011)

Optimum programs of correction of quasielliptical and circular orbits of spacecraft with the limited-thrust engine

Khramov A.A.

(Rus)

Vol 9, No 1 (2010)

Solving the problem of stabilizing program deployment of an orbital tether system taking into account limitations on the rotary motion of the tip body

1 1., 1 1.

(Rus)

Vol 12, No 4 (2013)

The usage of high power supply capacity transport spacecraft

Ivanovich S.N.

(Rus)

Vol 20, No 3 (2021)

Analysis of characteristics of electric propulsion systems intended for carrying out maneuvers of maintenance of low Earth working orbit of small satellites

Salmin V.V., Volotsuev V.V., Nikitin A.V.

(Rus)

Vol 18, No 2 (2019)

Determining the dynamics of spacecraft rotational motion with the use of information provided by global navigation satellite systems

Belokonov I.V., Kramlikh A.V., Lomaka I.A.

(Rus)

Vol 16, No 3 (2017)

Protocols of stitching image strips formed by optoelectronic converters and their application

Kuznetsov P.K., Martem’ianov B.V., Miatov G.N., Yudakov A.A.

(Rus)

Vol 15, No 2 (2016)

Procedure of comparative assessment of the efficiency of Earth remote sensing satellites with different optoelectronic telescopic complexes

Stratilatova N.N., Kurenkov V.I., Kucherov A.S., Egorov A.S.

(Rus)

Vol 10, No 6 (2011)

Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components

Titov B.A., Koltsov I.V.

(Rus)

Vol 14, No 1 (2015)

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.

(Rus)

Vol 11, No 4 (2012)

Dynamics of spacecraft landing in the area of its contact with the surface

Voronin V.V.

(Rus)

Vol 10, No 1 (2011)

Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits

Fadeenkov P.V., Ishkov S.A.

(Rus)

Vol 8, No 3-3 (2009): Special Issue

Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS

1 1., 1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 12, No 4 (2013)

Software and algorithmic support for the ground-based complex for small spacecraft attitude determination

Grigoryeva M.Y., Kramlikh A.V.

(Rus)

Vol 20, No 1 (2021)

Algorithm for solving optimal open-loop terminal control problem for spacecraft rendezvous with account of constraints on the state

Shorikov A.F., Goranov A.Y.

(Rus)

Vol 18, No 2 (2019)

Reducing the influence of interference of spacecraft magnetic field on magnetic measurements

Beznyakov A.M., Guriev I.S., Ryzhova I.P.

(Rus)

Vol 16, No 3 (2017)

Locally optimal control of space tug motion between the libration points of the Earth-Moon system

Starinova O.L., Fain M.K.

(Rus)

Vol 15, No 2 (2016)

Metodological basis of the development of a problem-oriented system for selecting design parameters of space vehicles

Stratilatov N.R., Kurenkov V.I., Kucherov A.S., Yakishik A.A.

(Rus)

Vol 14, No 4 (2015)

Optimization of spatial turns of «AIST-2» small spacecraft on the basis of the principle of minimum control

Petrishchev V.F., Shipov M.G.

(Rus)

Vol 14, No 1 (2015)

Analytical evaluation of the accuracy of spacecraft autonomous navigation according to the results of flight altitude adaptive measurement

Golyakov A.D., Fominov I.V.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

Comparative evaluation of the effectiveness of the application of perspective types of electric propulsion thrusters in the small spacecraft

Kulkov V.M., Obukhov V.A., Yegorov Y.G., Belik A.A., Krainov A.M.

(Rus)

Vol 9, No 4 (2010)

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.

(Rus)

Vol 7, No 2 (2008)

Methods and models of autonomous control over Earth remote sensing spacecraft survivability

Akhmetov R.N.

(Rus)

Vol 12, No 4 (2013)

Choosing the place for the installation of navigation system aerials on the ERS spacecraft body

Akhmetov R.N., Kurenkov V.I., Stratilatov N.R., Shilov L.B., Gordeev A.I.

(Rus)

Vol 19, No 3 (2020)

Design of control moment gyro electric drive with strict requirements on ensuring desired rotational velocities

Polozhentcev D.S., Davidov A.A., Shipov M.G., Kazakov E.P., Malykh B.I.

(Rus)

Vol 18, No 1 (2019)

Investigation of the technology of mutual navigation and orientation of small space vehicles flying in formation

Nebylov A.V., Perliouk V.V., Leontieva T.S.

(Rus)

Vol 16, No 3 (2017)

Construction of an upper stage flight pattern for placing a group of spacecraft into an orbit plane with the required angular distance between the satellites

Poplevin A.S., Panov N.A.

(Rus)

Vol 15, No 2 (2016)

СWSME – complex of wide-swath multispectral equipment for the «Resource-P» spacecraft

Baklanov A.I., Afonin A.N., Blinov V.D., Zabiyakin A.S.

(Rus)

Vol 14, No 4 (2015)

Procedure of accomodation of earth remote sansing satellite external devices with regard for the satellite target operation

Akhmetov R.N., Shilov L.B., Kurenkov V.I., Yakischik A.A.

(Rus)

Vol 14, No 1 (2015)

Development of a solar battery orientation robot system for small spacecraft

Beznyakov A.M., Vlasov V.A., Malenin E.N.

(Rus)

Vol 11, No 2 (2012)

Methods of protecting unpressurized compartments of spacecraft from the penetration of electromagnetic field

Syomkin N.D., Balakin V.L., Bragin V.V.

(Rus)

Vol 9, No 4 (2010)

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.

(Rus)

Vol 12, No 1 (2013)

Peculiarities of acoustic loading of the space vehicle in the nose fairing launched as part of a «Soyuz»-type rocket

Popov P.A., Sindyukov A.A., Kryuchkov A.N.

(Rus)

Vol 19, No 1 (2020)

Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor

Shipov M.G., Steklova A.A., Davydov A.A.

(Rus)

Vol 18, No 1 (2019)

Convective current experiments using Dakon-P equipment onboard “Progress” cargo spacecraft

Ayukaeva D.M., Babushkin I.A., Belyaev M.Y., Zilberman Y.A., Matveeva T.V., Sidorov A.S.

(Rus)

Vol 16, No 3 (2017)

Peculiarities of using additional low-power energy sources in the power supply system of small spacecraft

Kargu D.L., Beznyakov A.M., Nemirov A.V., Radionov N.V., Chudnovsky Y.A.

(Rus)

Vol 15, No 1 (2016)

System approach to the choice of capacity of a high-speed radio data link for modern Earth remote sensing spacecraft

Kascheev A.A.

(Rus)

Vol 14, No 4 (2015)

Bypass as an attribute of unmanned spacecraft operability in anomalous flight situations

Akhmetov R.N., Makarov V.P., Sollogub A.V.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Development of a prototype of a multi-loop closedbrayton cycle gas turbine power system

Arbekov A.N., Novitskiy B.B.

(Rus)

Vol 11, No 2 (2012)

Simulating electromagnetic field distribution due to electrostatic discharge on the spacecraft surface

Syomkin N.D., Balakin V.L., Bragin V.V.

(Rus)

Vol 9, No 2 (2010): Special Issue

Usage of the graphical languages in lifecycle of embedded software for spacecrafts

1 1., 1 1.

(Rus)

Vol 12, No 1 (2013)

Determination of optimum plans of Earth Remote Sensing spacecraft detailed survey by the use of a graph

Buzuev K.V.

(Rus)

1 - 89 of 89 Items

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