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Mathematical model of the aircraft optimal control under conditions of counteracting to a multiposition complex information-search system using the maximum undetection probability criterion

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Abstract

Mathematical model of the aircraft optimal control ensuring the probability maximization of its undetection by a group of measuring and search points forming part of a multiposition complex information-search system was obtained. To solve the problem, a model of search efforts specification was used where the control of each measuring and search terminal was assumed to be known.

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Authors and Affiliations

  1. Rostov Military Institute of Rocket Forces, Russia

    A. A. Strotsev, I. V. Shcherban’, S. A. Funtikov & V. A. Bertenev

Authors
  1. A. A. Strotsev
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  2. I. V. Shcherban’
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  3. S. A. Funtikov
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  4. V. A. Bertenev
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Additional information

Original Russian Text © A.A. Strotsev, I.V. Shcherban’, S.A. Funtikov, V.A. Bertenev, 2007, published in Izv. Vyssh. Uchebn. Zaved., Radioelektron., 2007, Vol. 50, No. 9, pp. 34–42.

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Strotsev, A.A., Shcherban’, I.V., Funtikov, S.A. et al. Mathematical model of the aircraft optimal control under conditions of counteracting to a multiposition complex information-search system using the maximum undetection probability criterion. Radioelectron.Commun.Syst. 50, 491–496 (2007). https://doi.org/10.3103/S0735272707090063

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  • DOI: https://doi.org/10.3103/S0735272707090063

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