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An algorithm for constructing a control function that transfers a wide classof stationary nonlinear systems of ordinary differential equations from aninitial state to a final state under certain control restrictions is proposed.The algorithm is designed to be convenient for numerical implementation. Aconstructive criterion of the desired transfer possibility is presented. Theproblem of an interorbital flight is considered as a test example and it issimulated numerically with the presented method.

Solving Boundary Value Problem for a Nonlinear Stationary Controllable System with Synthesizing Control