Physics
Scientist
Constructing a Spatial Attainability Region for a Spacecraft Entering the Atmosphere with Near-Circular Velocity and a Large Entry Angle
On Constructing the Attainability Region at the Earth's Surface for a Spacecraft with Constraints on Phase Coordinates
On Constructing the Region of Reducibility to a Specified Point for a Spacecraft Entering the Atmosphere
Solution of optimal-control problems for atmospheric entry
Some Properties of Optimal Ricochet Trajectories at Spacecraft Entry into the Atmosphere
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