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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 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)

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 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 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 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 16, No 3 (2017)

Iteration procedure of choosing a low-thrust rendezvous transfer control program in problems of space debris disposal in the geostationary orbit

Philippov G.A.

(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 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 8, No 4 (2009)

History of small space vehicle progress and development at Plesetsk cosmodrome. Current problems of further development

Korotkov V.V., Vinogradov A.V.

(Rus)

Vol 21, No 3 (2022)

Two-channel optimal discrete law of control of spacecraft with aerodynamic and inertial asymmetry during descent in Mars atmosphere

Lyubimov V.V., Bakry I.

(Rus)

Vol 18, No 4 (2019)

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

Shornikov A.Y.

(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)

Development of small satellite structure taking into account the use of laser measuring systems

Shaposhnikov S.N.

(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 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)

Concept of multilevel adaptation of integrated navigation systems of small spacecraft

Fominov I.V.

(Rus)

Vol 11, No 7 (2012)

Calculation of the electromagnetic field in homogeneous hull of on board equipment of space vehicle under influence of electrostatic discharges

Kostin A.V.

(Rus)

Vol 14, No 3 (2014)

Stochastic method of investigating perturbed motion of a space vehicle in the atmosphere

Sokolov N.L.

(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

Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust

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

(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 1 (2013)

Integrated assessment of the efficiency of an orbital inspection space system based on small satellites

Tkachenko I.S., Kaurov I.V.

(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 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 4 (2018)

Development of methods for ensuring energy balance for the operation of mission equipment of “AIST”-series small satellites under conditions of power limitations

Ivanushkin M.A., Salmin V.V., Tkachenko S.I., Tkachenko I.S., Volgin S.S.

(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)

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 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 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 13, No 1 (2014)

Constructive actions for decreasing the acoustic pressure inside space-rocket products

Popov P.A., Sindyukov A.A.

(Rus)

Vol 9, No 2 (2010): Special Issue

The design shape and basic performances of small satellite of SSAU and SRP SRC “TSSKB-Progress”

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

(Rus)

Vol 8, No 2 (2009)

Dependence of the extent to which the space vehicle’s own atmosphere and plasma generated by stationary plasma engines affect the space vehicle on its structural lay-out

Testoyedov N.A., Smirnov V.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 21, No 1 (2022)

Isotopy of spacecraft compartment hull shapes

Belyakov A.A., Shulepov A.I.

(Rus)

Vol 17, No 3 (2018)

Refinement of operable state recovery algorithms for “AIST” small satellites on the basis of telemetric information

Volgin S.S., Salmin V.V., Tkachenko S.I., Tkachenko I.S., Ivanushkin M.A.

(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 10, No 7 (2011)

The analysis of methods of protection of onboard equipment of space vehicles from influence of factors of the electrostatic discharge

Kostin A.V.

(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)

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 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 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 2 (2010): Special Issue

Ways of the development of the radar space systems of the remote sensing of the Earth

1 1.

(Rus)

Vol 8, No 1 (2009)

Experiments aboard the space vehicle “Photon-M” NO.3 and some reseelts of the mission

Abrashkin V.I., Shatokhin S.M., Kovalyova T.B., Safronov S.L.

(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)

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)

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

Shipov M.G.

(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 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 2 (2016)

Application of simulation modelling in static tests of space-rocket vehicles

Grebnev D.N., Duplihin V.K., Zuperman J.A., Aistov A.I., Kukushkin V.E.

(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)

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 11, No 2 (2012)

Choice of design parameters of universal platforms of small space vehicles

Volotsuev V.V., Tkachenko I.S., Safronov S.L.

(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 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 7, No 3 (2008): Special Issue

Ground testingresults of loop heat pipe used to maintain thermal conditions of equipment

Biryuk V.V., Kitaev 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 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)

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 2 (2016)

Analysis of the accuracy of Earth remote sensing satellite angular motion control and track guidance during route observation intervals

Galkina A.S., Platoshin I.V.

(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 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 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 7, No 1 (2008)

System of artificial intellect support of low-thrust spacecraft interplanetary mission optimization

Starinova O.L.

(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 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 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 14, No 4 (2015)

Flight development tests and attempted operation of «AIST» small satellites

Kirilin A.N., Tkachenko S.I., Salmin V.V., Semkin N.D., Papkov A.P., Abrashkin V.I., Tkachenko I.S., Zheleznov Y.E., Galaeva E.Y.

(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 4 (2012)

Peculiarities of Earth observation space vehicle control in contingencies

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

(Rus)

Vol 11, No 1 (2012)

Visual approach to verifictaion of real-time control software

Tyugashev A.A., Bogatov A.Y., Shulyndin A.V.

(Rus)

Vol 9, No 2 (2010): Special Issue

Creation of infotainment support of designing of control algorithms logic of spacecraft onboard control complexeses

1 1.

(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 7, No 1 (2008)

Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II

Salmin V.V., Vassiliev V.V., Ishkov S.A., Romanenko V.A., Sokolov V.O., Starinova O.L., Yurin V.V.

(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 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)

Russian-Azerbaijani space project of a small satellite for science and technology experiments

Samedov A.S., Panasyuk M.I., Abdulaev P.S., Bogomolov V.V., Gasanov R.A., Ibragimov R.A., Iyudin A.F., Mammadzada T.G., Musaev A.A., Osedlo V.I., Petrov V.L., Podzolko M.V., Popova E.P., Rustamov R., Svertilov S.I., Seiidov H., Yashin I.V.

(Rus)

Vol 16, No 4 (2017)

Сonceptual design of small spacecraft with a high resolution P-VHF band bistatic SAR system

Goryachkin O.V., Maslov I.V., Zhengurov B.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 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 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 4 (2012)

Selection of sites and angles for placing star coordinators of remote sensing satellites

Akhmetov R.N., Kurenkov V.I., Stratilatov N.R., Fedorenko O.G., Shilov L.B.

(Rus)

Vol 13, No 2 (2014)

Calculation of power dissipation in corps of onboard equipment of space vehicle in direct electrostatic discharge

Kostin A.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 8, No 4 (2009)

Vibration resistance problem for a space vehicle with single-degree-of-freedom powered gyroscopes

Filippov Y.I., Peresypkin K.V.

(Rus)

Vol 7, No 1 (2008)

Orbital tether system motion equations considering space vehicle vibrations

Aslanov V.S., Stratilatov N.R.

(Rus)

Vol 12, No 4 (2013)

The usage of high power supply capacity transport spacecraft

Ivanovich S.N.

(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 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 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 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)

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