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.
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.
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.
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.
Accuracy of autonomous navigation by the mutual method in the case of a group flight of space vehicles
Golyakov A.D., Richnyak A.M.
Concept of multilevel adaptation of integrated navigation systems of small spacecraft
Fominov I.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.
Small spacecraft for the registration of micrometeorites and space debris
Semkin N.D., Telegin А.М., Vidmanov A.S.
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.
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.
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Zabolotnov Y.M., Lobankov A.A.
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.
Software and algorithmic support for the ground-based complex for small spacecraft attitude determination
Grigoryeva M.Y., Kramlikh A.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.
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.
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.
Optimization of spatial turns of «AIST-2» small spacecraft on the basis of the principle of minimum control
Petrishchev V.F., Shipov M.G.
1 - 17 of 17 Items

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