Physics
Scientist
Automatic Optimization of the Flight of a Space Vehicle for a Regime Corresponding to Maximum Aerodynamic Performance
Certain problems in Controlling the Banking of a Spacecraft in the Atmospheric Reentry Phase
Control of Spacecraft at Re-entry intothe Atmosphere by Means of Variable-Structure Systems
Control of the Attack Angle of a Spacecraft by Varying the Centering
The Problem of Optimal Control for the Descent of a Space Vehicle in the Atmosphere
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