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Found 736 Documents (Results 1–100)

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Optimal orientation control of a space vehicle with restrictions on the control and phase variables. (English. Russian original) Zbl 1487.49058

J. Comput. Syst. Sci. Int. 60, No. 6, 1027-1045 (2021); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2021, No. 6, 158-176 (2021).
MSC:  49S05 49K21
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Studying the accuracy of forecasting electric power generation by solar panels of the Zarya service module on the international space station using a mathematical model. (English. Russian original) Zbl 1484.78010

Mosc. Univ. Comput. Math. Cybern. 45, No. 4, 180-190 (2021); translation from Vestn. Mosk. Univ., Ser. XV 2021, No. 4, 43-52 (2021).
MSC:  78A55 78A40 65K10
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Determining the parameters of a mathematical model of spacecraft solar batteries from telemetry data. (English. Russian original) Zbl 07441911

Mosc. Univ. Comput. Math. Cybern. 45, No. 3, 120-125 (2021); translation from Vestn. Mosk. Univ., Ser. XV 2021, No. 3, 37-43 (2021).
MSC:  65Kxx 90Cxx 90-XX
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Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional. (English. Russian original) Zbl 1475.49023

Autom. Remote Control 82, No. 7, 1183-1200 (2021); translation from Avtom. Telemekh. 2021, No. 7, 86-106 (2021).
MSC:  49K15 49K21
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Analytical algorithm of energy and time quasioptimal turn of a spacecraft under arbitrary boundary conditions. (Russian. English summary) Zbl 1464.70019

MSC:  70M20 70Q05
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Methodology of intelligent analysis and forecasting for the state of resources in the Russian segment of the international space station based on digital identification models. (English. Russian original) Zbl 1454.93159

Autom. Remote Control 81, No. 9, 1692-1701 (2020); translation from Avtom. Telemekh. 2020, No. 9, 160-172 (2020).
MSC:  93C62 93C95
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Comparison of two models of the force of aerodynamic drag for determining the orbital motion of the International Space Station. (Russian. English translation) Zbl 1493.70086

Mat. Model. 32, No. 10, 77-90 (2020); translation in Math. Models Comput. Simul. 13, No. 3, 502-511 (2021).
MSC:  70M20
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Synthesis of the optimal control of the spacecraft orientation using combined criteria of quality. (English. Russian original) Zbl 1448.93087

J. Comput. Syst. Sci. Int. 58, No. 6, 980-1003 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 6, 139-162 (2019).
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Analytical algorithm for constructing the orbital orientation of a spacecraft with an incomplete measurement of the state vector components. (English. Russian original) Zbl 1448.93089

J. Comput. Syst. Sci. Int. 58, No. 6, 969-979 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 6, 128-138 (2019).
MSC:  93B50 93B53 93C95
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Algorithm for controlling a spacecraft’s engine with preventing the angular momentum accumulation. (English. Russian original) Zbl 1440.93181

J. Comput. Syst. Sci. Int. 58, No. 5, 801-810 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 5, 145-154 (2019).
MSC:  93C95 93C27
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Calculation of program controls not generating singular states of a gyro system. II. (English. Russian original) Zbl 1432.93245

J. Comput. Syst. Sci. Int. 58, No. 3, 491-502 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 3, 164-176 (2019).
MSC:  93C95 93-08
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Algorithms of stabilization of a spacecraft with flexible elements. (English. Russian original) Zbl 1432.93262

J. Comput. Syst. Sci. Int. 58, No. 3, 474-490 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 3, 147-163 (2019).
MSC:  93D05 93C95
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Reconstruction of a spacecraft’s attitude motion using the data on the current collected from solar panels. (English. Russian original) Zbl 1432.93244

J. Comput. Syst. Sci. Int. 58, No. 2, 286-296 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 2, 133-144 (2019).
MSC:  93C95
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Restricted quadratic optimal control of a spacecraft turning in a fixed time period. (English. Russian original) Zbl 1432.49069

J. Comput. Syst. Sci. Int. 58, No. 1, 126-146 (2019); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upravl. 2019, No. 1, 131-152 (2019).
MSC:  49S05 49K15 70G75
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Optimal rotation of the orbit plane of a variable mass spacecraft in the central gravitational field by means of orthogonal thrust. (English. Russian original) Zbl 1431.93032

Autom. Remote Control 80, No. 8, 1437-1454 (2019); translation from Avtom. Telemekh. 2019, No. 8, 87-108 (2019).
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