Simulating the process of retargeting of optoelectronic Earth observation spacecraft during object shooting
Kurenkov V.I., Pupkov E.A., Kucherov A.S.
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.
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.
Automated generation of structural members of a spacecraft thermal model
Kulikov D.S., Shatin A.A., Velmisov I.G.
Isotopy of spacecraft compartment hull shapes
Belyakov A.A., Shulepov A.I.
Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem
Tsaplin S.V., Bolychev S.A.
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.
Reducing the influence of interference of spacecraft magnetic field on magnetic measurements
Beznyakov A.M., Guriev I.S., Ryzhova I.P.
Locally optimal control of space tug motion between the libration points of the Earth-Moon system
Starinova O.L., Fain M.K.
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.
Optimization of spatial turns of «AIST-2» small spacecraft on the basis of the principle of minimum control
Petrishchev V.F., Shipov M.G.
Analytical evaluation of the accuracy of spacecraft autonomous navigation according to the results of flight altitude adaptive measurement
Golyakov A.D., Fominov I.V.
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.
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.
Methods and models of autonomous control over Earth remote sensing spacecraft survivability
Akhmetov R.N.
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.
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.
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.
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.
СWSME – complex of wide-swath multispectral equipment for the «Resource-P» spacecraft
Baklanov A.I., Afonin A.N., Blinov V.D., Zabiyakin A.S.
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.
Development of a solar battery orientation robot system for small spacecraft
Beznyakov A.M., Vlasov V.A., Malenin E.N.
Methods of protecting unpressurized compartments of spacecraft from the penetration of electromagnetic field
Syomkin N.D., Balakin V.L., Bragin V.V.
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.
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.
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.
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.
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.
System approach to the choice of capacity of a high-speed radio data link for modern Earth remote sensing spacecraft
Kascheev A.A.
Bypass as an attribute of unmanned spacecraft operability in anomalous flight situations
Akhmetov R.N., Makarov V.P., Sollogub A.V.
Development of a prototype of a multi-loop closedbrayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Simulating electromagnetic field distribution due to electrostatic discharge on the spacecraft surface
Syomkin N.D., Balakin V.L., Bragin V.V.
Usage of the graphical languages in lifecycle of embedded software for spacecrafts
1 1., 1 1.
Determination of optimum plans of Earth Remote Sensing spacecraft detailed survey by the use of a graph
Buzuev K.V.
Optimal control of spacecraft motion in the vicinity of Eros 433 asteroid
Shornikov A.Y.
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.
Small spacecraft for the registration of micrometeorites and space debris
Semkin N.D., Telegin А.М., Vidmanov A.S.
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.
Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine
Ishkov S.A., Filippov G.A.
Methods of measurement and calculation of microaccelerations onboard of low orbit space microgravitational platform
1 1., 1 1., 1 1.
Improvements in methods of analysis and control of space-rocket equipment reliability at the stage of complex electrical testing
Belova V.V.
Influence of space vehicle remote power supply on thermal regimes of solar batteries
Steganov G.B., Beznyakov A.M., Nemirov A.V.
Control program for noncoplanar heliocentric flight to Venus of non-perfectly reflecting solar sail spacecraft
Khabibullin R.M.
Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft
Igolkin A.A., Safin A.I., Filipov A.G.
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.
Results of operation of scientific hardware «Space system of microacceleration compensation»
Semkin N.D., Piyakov I.V.
Concept of multilevel adaptation of integrated navigation systems of small spacecraft
Fominov I.V.
Synthesis of dynamic modes of attitude motion of spacecraft with solid propellant rocket engine
Balakin V.L., Doroshin A.V., Krikunov M.M.
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.
The rotation maneuvers and synthesis of gyromoment guidance laws for land-survey spacecraft
1 1., 1 1., 1 1.
Method of calculating self-capacitance in planar structural elements of a spacecraft
Syomkin N.D., Bragin V.V., Pomelnikov R.A., Balakin V.L.
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.
Accuracy of autonomous navigation by the mutual method in the case of a group flight of space vehicles
Golyakov A.D., Richnyak A.M.
Spacecraft power supply system using additional low-power sources of energy
Kargu D.L., Beznyakov A.M., Nemirov A.V.
Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit
Ishkov S.A.
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.
Method of choosing spacecraft design characteristics on the basis of creating task-oriented systems of computer-aided design
Kucherov A.S., Kurenkov V.I.
Problems of unmanned spacecraft reengineering in abnormal flight situations and their knowledge-based solutions
Akhmetov R.N., Makarov V.P., Sollogub A.V.
Choosing the structure of power-supply systems for low-orbit space vehicles
1 1., 1 1., 1 1., 1 1.
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.
Estimation and analysis of the influence of ionizing radiation on the operation of nanosatellite onboard radio electronic equipment
Tsaplin S.V., Bolychev S.A.
Reduction of angular velocities of AIST-2D spacecraft using a system of kinetic moment dumping
Shipov M.G.
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.
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Zabolotnov Y.M., Lobankov A.A.
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.
Adaptive algorithm of determining low altitude spacecraft orientation on the basis of processing instant diverse-type measurements
Grigoryeva M.Y., Kramlikh A.V.
Optimum programs of correction of quasielliptical and circular orbits of spacecraft with the limited-thrust engine
Khramov A.A.
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.
The usage of high power supply capacity transport spacecraft
Ivanovich S.N.
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.
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.
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.
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.
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.
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.
Dynamics of spacecraft landing in the area of its contact with the surface
Voronin V.V.
Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits
Fadeenkov P.V., Ishkov S.A.
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.
Software and algorithmic support for the ground-based complex for small spacecraft attitude determination
Grigoryeva M.Y., Kramlikh A.V.
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