Lateral guidance of a spacecraft in the atmosphere

Physics

Scientific paper

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Atmospheric Entry, Lateral Control, Reentry Guidance, Spacecraft Guidance, Spacecraft Reentry, Algorithms, Differential Equations, Roll, Spacecraft Maneuvers, Trajectory Control

Scientific paper

The problem of the lateral guidance of a spacecraft during reentry is
examined with allowance for constraints on the number of roll reversals.
A lateral-guidance algorithm is proposed which is based on the
construction of attainability regions in the space of finite parameters.
The application of this algorithm is illustrated by numerical examples.

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