Archive

Volume 4, No. 3(33), 2020

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

129-140

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

141-150

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

151-160

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

161-170

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

171-177

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

178-185

Volume 4, No. 2(32), 2020

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

61-71

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

72-84

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

85-95

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

96-106

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

107-115

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

116-122

Volume 4, No. 1(31), 2020

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

5-13

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

14-19

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

20-27

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

28-35

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

36-44

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

45-54