Abstract:
An easy-to-implement numerical method is proposed for synthesizing a feedback control function that transfers a wide class of nonlinear stationary systems from an initial state to a given terminal state with allowance for measured data. A constructive criterion is obtained for choosing terminal states for which this transfer is guaranteed. The problem of an interorbital flight is considered and numerically simulated.
Key words:nonlinear control system, synthesis of feedback control functions, numerical implementation of synthesis, asymptotic observer.
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