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Title
Authors
Methodology of designing a space transport system including a “DM” chemical upper stage and an electric rocket transport module
Russkikh A.S., Salmin V.V.
Method of automated arrangement of devices in a spacecraft compartment taking into account connection to interface connectors of feed-through plates of an on-board cable system
Belyakov A.A., Prihodko V.I., Shulepov A.I.
History of small space vehicle progress and development at Plesetsk cosmodrome. Current problems of further development
Korotkov V.V., Vinogradov A.V.
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.
Choice of mission trajectory plans and conceptual design of electrical propulsion module for launching payloads into circumterrestrial orbits
Salmin V.V., Kvetkin A.A., Russkikh A.S.
Arrangement of data for the formation of a multidimensional array of essential insights in automated enterprise management system
Kartamyshev A.S.
Influence of space vehicle remote power supply on thermal regimes of solar batteries
Steganov G.B., Beznyakov A.M., Nemirov A.V.
Information control system for space experiments onboard international space station
Voronin F.A., Dunaeva 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.
Choice of design parameters of universal platforms of small space vehicles
Volotsuev V.V., Tkachenko I.S., Safronov S.L.
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
Efficiency of terminal control in the trans-atmospheric first stage of an aerospace system under atmospheric and aerodynamic disturbances
Balakin V.L., Kovalyov A.V., Krikunov M.M.
Modelling the architecture of a system controlling the condition of maintenance objects
Koptev A.N., Yergaliyev D.S., Sakhanov K.Z.
Experimental simulation of registration of outer space objects
Baryshev Y.Y., Syomkin N.D., Voronov K.Y.
The usage of high power supply capacity transport spacecraft
Ivanovich S.N.
Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
Ananenko V.M., Golyakov A.D., Kalabin P.V.
Analysis of motion stability of a deployed space tether system with an atmospheric probe
Zhe D., Zabolotnov Y.M., Changqing W.
Control over maintaining accuracy of integrity of reference surfaces of spacecraft components in their joint functioning at various stages of design
Yelenev V.D., Schuplyak Y.P.
Methods of validation of the ballistic structure of space surveillance system orbital segment
Fadin I.A., Yanov S.V., Samokhvalov O.A.
Ways of the development of the radar space systems of the remote sensing of the Earth
1 1.
Analytical determination of motion parameters of the center of mass of an uncooperative orbiter on the basis of measurement information provided by on-board systems of a space robot in a coplanar orbit
Ananenko V.M., Golyakov A.D., Kalabin P.V.
Locally optimal control of space tug motion between the libration points of the Earth-Moon system
Starinova O.L., Fain M.K.
Building foundations of virtual information-based educational environment
Zelenko L.S., Zagumennov D.A., Zinchenko A.O.
The influence of tether jamming on the motion of a space tether system during dynamic deployment
Ledkov A.S., Dyukov D.I.
Integrated assessment of the efficiency of an orbital inspection space system based on small satellites
Tkachenko I.S., Kaurov I.V.
1 - 25 of 25 Items

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