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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.
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.
Estimating the design parameters of a space-based radio surveillance system
Ivanushkin M.A., Zhaldybina O.D., Safronov S.L., Korovin M.D.
Small spacecraft for the registration of micrometeorites and space debris
Semkin N.D., Telegin А.М., Vidmanov A.S.
Сonceptual design of small spacecraft with a high resolution P-VHF band bistatic SAR system
Goryachkin O.V., Maslov I.V., Zhengurov B.G.
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.
Software and algorithmic support for the ground-based complex for small spacecraft attitude determination
Grigoryeva M.Y., Kramlikh A.V.
Development of small satellite structure taking into account the use of laser measuring systems
Shaposhnikov S.N.
Concept of multilevel adaptation of integrated navigation systems of small spacecraft
Fominov I.V.
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.
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.
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.
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.
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.
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.
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.
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.
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.
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Zabolotnov Y.M., Lobankov A.A.
Choice of design parameters of universal platforms of small space vehicles
Volotsuev V.V., Tkachenko I.S., Safronov S.L.
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.
Optimization of spatial turns of «AIST-2» small spacecraft on the basis of the principle of minimum control
Petrishchev V.F., Shipov M.G.
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.
Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft
Igolkin A.A., Safin A.I., Filipov A.G.
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.
Integrated assessment of the efficiency of an orbital inspection space system based on small satellites
Tkachenko I.S., Kaurov I.V.
1 - 26 of 26 Items

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