Archive

Volume 3, No. 4(30), 2019

Taygin V.B., Lopatin А.V.
Method of achievement the high accuracy of the shape of reflectors of mirror antennas of spacecraft

200-208

Lukonin N.V., Golovenkin E.N., Dmitriev G.V., Shestakov I.Ya.
Increase of efficiency of actuators of spacecraft thermal control system in outer space

209-215

Starostin E.A., Lebedev A.P., Moskovskih M.S., Maslov E.P.
Development of technology to ensure minimal thermal resistance between mating surfaces while simulating outer space conditions

216-221

Azin A.V., Kuznetsov S.A., Ponomarev S.A., Ponomarev S.V., Rikkonen S.V.
Simulation of contact interaction of piezoelectric engine elements

222-229

Chebotarev V.E., Salomatov Yu.P., Panko V.S., Erokhin A.A., Kuzmin E.V., Ryazantsev R.O.
The satellite distance radiometer with a passive retroreflection of a request radio signal

230-236

Vladimirov V.M., Ratushnyak V.N., Vyakhirev V.A., Tyapkin I.V.
Features of scanning the atmosphere and building radar stations of vertical sounding with a low-element antenna array

237-242

Volume 3, No. 3(29), 2019

Taygin V.B., Lopatin А.V.
Design of the mirror antenna of a spacecraft with the ultralight high precision size-stable reflector

121-131

Ivanov D.S., Meus S.V., Nuralieva A.B., Ovchinnikov A.V., Ovchinnikov M.Yu., Roldugin D.S., Tkachev S.S., Shestoperov A.I., Shestakov S.A., Yakimov E.N.
Attitude control and determination algorithms for the spacecraft with two flexible appendages

132-139

Moskvichev V.V., Lepikhin A.M., Burov A.E., Doronin S.V., Moskvichev E.V.
Calculation and experimental assessment of the strength and limit states of composite structures for spacecraft

140-148

Chubar A.V., Pozharkova I.N., Ustimenko V.V.
Creation of control algorithms thermal vacuum tests in the SimInTech environment

149-154

Yakovlev O.Ya., Malygin D.V.
External thermal modeling satellite platform «Synergy»

155-163

Azin A.V., Kuznetsov S.A., Ponomarev S.A., Ponomarev S.V., Rikkonen S.V.
Mathematical modeling of piezoelectric step-engine work

164-170

Gornostaev A.I.
Optimization of the structure of the unified multichannel interface temperature control module for measuring instruments of spacecraft

171-183

Volume 3, No. 2(28), 2019

Berdnikova N.А., Belov O.А., Lopatin А.V.
Research and optimization of production cycle of high-precision composite spacecraft antenna reflector

59-72

Ovchinnikov M.Yu., Roldugin D.S.
Recent advances in the active magnetic control of satellites

73-86

Kovel A.A.
Prognostic potential of mathematical experiment planning

87-93

Utkin M.N., Saybel A.G.
Modernization of time scale control unit for «Glonass-K2» spacecrafts

94-100

Kovalyov R.B., Ratushnyak V.N., Zverev P.Yu.
Research of parameters and calculation of the budget of the radio line in the ground-based system of near navigation on the basis of pseudo-satellites

101-106

Chebotarev V.E., Sidorova I.L.
Space technologies – one of the basic bases of innovative development of the siberian region

107-113

Volume 3, No. 1(27), 2019

Shilko I.I., Voloshko Yu.B., Ruzhilova O.V., Anisimova O.A.
Analysis of upgrade options for the structure of orbital grouping of the GLONASS system to ensure its competitiveness

5-12

Dvirniy V.V., Krushenko G.G., Dvirniy G.V., Shevchuk A.A., Elfimova M.V., Kuznetsova M.S.
Features of components of spacecraft thermal control systems

13-21

Myznikova V.A., Ustimenko V.V., Chubar A.V.
Fuzzy controllers construction in the SimInTech environment

22-27

Shevchuk A.A., Dvirniy G.V., Krushenko G.G., Dvirniy V.V., Elfimova M.V.
Optical system of perspective led-based solar simulator for spacecraft ground testing applications

28-40

Gornostaev A.I.
Problems of unification of multi-channel interface temperature control module for measuring instruments of spacecraft

41-51