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Integrated aircraft control for rendezvous of aircraft-launched missiles with radiating targets

  • Control Systems of Moving Objects
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Journal of Computer and Systems Sciences International Aims and scope

Abstract

This paper solves the problem of rendezvous of an aircraft-launched missile with a maneuvering radiating target so as to maximize the launch range (agreed launch conditions). The information maneuver (vertical, horizontal, and spatial) of the aircraft that maximally improves the accuracy of radiating target tracking and is executed before the aircraft meets the agreed launch conditions is determined. An algorithm for determining the current demands for aircraft control with respect to bank angle and load factor is developed to solve the problem of rendezvous with each tracked target. The integrated aircraft control is based on choosing a priority target at the current time and supplying the current control demand in terms of the desired bank angle and load factor.

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References

  1. Control Ssystems of Fighter Aircraft Weapobry, Ed. by E.A. Fedosov (Mashinostroenie, Moscow, 2005) [in Russian].

    Google Scholar 

  2. L. E. Shirokov, “Complex hypothesis tracking of moving objects,” J. Comput. Syst. Sci. Int. 39, 975–994 (2000).

    Google Scholar 

  3. A. N. Shiryaev, “New results in the theory of controlled stochastic processes,” in Proc. of the IV Prague Conf. on Information Theory, Statistical Decisions Functions, and Random Processes, Prague, 1967.

  4. A. Miele, Flight Mechanics (Addison-Wesley, Reading, Mass., 1962; Nauka, Moscow, 1965).

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  5. L. E. Shirokov, “Synthesis of optimal control in symmetric problems,” Izv. Akad. Nauk SSSR, Tekh. Kibern., No. 4 (1983).

    Google Scholar 

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Authors and Affiliations

  1. State Research Institute of Aviation Systems, ul. Viktorenko 7, Moscow, 125319, Russia

    L. E. Shirokov

Authors
  1. L. E. Shirokov
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Correspondence to L. E. Shirokov.

Additional information

Original Russian Text © L.E. Shirokov, 2014, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2014, No. 2, pp. 147–160.

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Cite this article

Shirokov, L.E. Integrated aircraft control for rendezvous of aircraft-launched missiles with radiating targets. J. Comput. Syst. Sci. Int. 53, 291–304 (2014). https://doi.org/10.1134/S1064230714020142

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  • DOI: https://doi.org/10.1134/S1064230714020142

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