Volume 4, No. 4(34), 2020

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Grishin V.I., Glebova M.A., Dudarkov Yu.I., Levchenko E.A., Limonin M.V.
Strength analysis of structural elements and metal-composite joints of a flying vehicle

Gladyshev A.B., Dmitriev D.D., Ratushnyak V.N., Zhgun A.V., Gritsan O.B.
Stand for measuring the directional characteristics of antennas of satellite communication systems

Golovanov S.M., Orlov V.I., Fedosov V.V.
Using the concepts of homogeneity in additional tests of electronic components for space applications

Krikunov I.L., Gaipov K.E.
Application of piecewise-linear approximation of probabilistic-time characteristics of queuing systems

Sukhotin V.V., Tikhtenko A.S., Zhgun A.V., Sidorin V.A.
Digital filter for device of determining coordinates of radio signal source in satellite telecommunications systems

Chebotarev V.E., Vorontsova E.O.
Method of providing energy resources to a circumlunar satellite for passing longduration shadow zones

Volume 4, No. 3(33), 2020

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Shevchuk A.A., Pastushenko O.V., Dvirniy V.V., Dvirniy G.V., Filatov A.A.
Problems of irradiance characteristics measurement of solar simulators for ground spacecraft tests

Khabibullin R.M., Starinova O.L.
Non-coplanar interplanetary flight simulation considering motion relative to the center of mass peculiarities of solar sail spacecraft

Soloviev S.V.
Justification of the choice of the method and criterion of clustering for intelligent analysis in flight control spacecraft

Starinova O.L., Sergaeva E.A., Shornikov A.Yu.
Design and ballistic analysis of the mission for long-term study of the asteroid Apophis by a nanosatellite with an electric rocket propulsion system

Mikhaylenko L.A., Rusin D.S., Ustimenko V.V., Chubar A.V.
Parametric synthesis of the controller by metaheuristic algorithm in the SimInTech environment

Mikhaylenko L.A., Ustimenko V.V., Chubar A.V.
Designing a control system for the orientation of solar panels in the dynamic simulation environment of SimInTech technical systems

Volume 4, No. 2(32), 2020

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Volotsuev V.V., Salmin V.V.
Analysis of the cyclogram of maintaining a low working orbit of a spacecraft of the AIST-2 class using an electric jet engine

Anshakov G.P., Krestina A.V., Tkachenko I.S.
Analysis of the effectiveness of the de-orbiting devices for small satellite

Kazantsev Z.A., Eroshenko A.M., Uvaev I.V., Lopatin A.V.
Parabolic transformable reflector for CubeSat platform

Gluzdov A.N., Gorbulin P.V., Kotyashov E.V., Kuvaev O.L.
Method of graphoanalytical finding borders space-time areas of reachability service spacecraft man-made space objects in geostationary orbit

Isaeva O.S., Nozhenkova L.F., Mishurov A.V., Kamyshnikov A.N., Evstratko V.V., Chernigovskiy A.S.
Creation of the spacecraft’s command-and-measurement system’s heterogeneous simulation model

Krat N.M.
Vector network analyzer usage at calibration of delay in satellite radio navigation system signal simulators

Volume 4, No. 1(31), 2020

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Khabibullin R.M.
Procedure for forming nominal control program of solar sail spacecraft heliocentric movement using locally optimal control laws

Asadov H.H., Mamedova U.F.
Questions on utilization of different height balloon sources of optical radiation for calibration of network of ground microtelescopes for tracking of orbital satellites

Prokhorov M.A., Tsvetkov A.Yu., Tolmachev A.A.
Development of an automated system for deploying software for automated workstations of the spacecraft flight control center

Zuev D.M., Okhotkin K.G.
Modified formulas for maximum deflection of a cantilever under transverse loading

Mikhalkin V.M., Pastushenko O.V., Dvirniy V.V., Dvirniy G.V., Shevchuk A.A.
Reducing operational costs of thermal vacuum testing of spacecraft via gaseous nitrogen thermal conditioning technology

Blinov V.V., Vladimirov V.M., Kushnarev N.A., Nikiforov A.I., Pridachin D.B., Pchelyakov D.O., Pchelyakov O.P., Skorodelov V.A., Sokolov L.V.
Growing semiconductor structures for high-performance solar cells in open space