Descent control in a disturbed atmosphere on the basis of a variational method for the synthesis of invariant systems

Physics

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Atmospheric Entry, Control Theory, Descent Trajectories, Spacecraft Control, Variational Principles, Algorithms, Atmospheric Density, Equations Of Motion, Perturbation Theory

Scientific paper

The variational theory of invariance is used to obtain a numerical solution to the problem of synthesizing an explicit control law for spacecraft descent in a disturbed atmosphere. This law provides for the absolute independence of the given quality index from atmospheric-density disturbances and certain parameters of the spacecraft. Results of simulation are presented for descent distance control in the disturbed atmosphere of the earth.

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