An Effective Algorithm of Aerodynamic Control over Spacecraft Descent

Computer Science

Scientific paper

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Scientific paper

An algorithm of aerodynamic control is suggested for the descent of a spacecraft with a small lift-to-drag ratio into a predetermined region of space. The algorithm provides for an oriented descent with accepted accuracy for a subsequent operation of the landing control system. It needs less computing in comparison with traditional algorithms due to reduction of the initial nonlinear boundary value problem to the Cauchy problem.

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