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Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor
Shipov M.G., Steklova A.A., Davydov A.A.
Two-channel optimal discrete law of control of spacecraft with aerodynamic and inertial asymmetry during descent in Mars atmosphere
Lyubimov V.V., Bakry I.
Design of control moment gyro electric drive with strict requirements on ensuring desired rotational velocities
Polozhentcev D.S., Davidov A.A., Shipov M.G., Kazakov E.P., Malykh B.I.
Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem
Tsaplin S.V., Bolychev S.A.
On-board algorithm for SamSat-218D nanosatellite orientation and stabilization system
Kramlikh A.V., Melnik M.E.
Analysis of the accuracy of Earth remote sensing satellite angular motion control and track guidance during route observation intervals
Galkina A.S., Platoshin I.V.
Improvement of the flight attitude control accuracy of the Earth observation spacecraft
Akhmetov R.N., Sollogub A.V., Makarov V.P., Golovchenko A.A., Filatov A.V.
CFD-based modeling of oil ang gas journal bearings using commercial software packages
Pugachev A.O., Ravikovich Y.A., Ermilov Y.I., Kholobtsev D.P., Matushkin A.A.
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