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Effects of Divert-Thrusters on Homing Performance of Endo-atmospheric Interceptors

Author

Listed:
  • Yanfang Liu

    (Harbin Institute of Technology)

  • Naiming Qi

    (Harbin Institute of Technology)

  • Zhiwei Tang

    (Harbin Institute of Technology)

Abstract

A new guidance law is proposed for interceptor missiles by using a differential game formulation with bounded controls. The interceptor is steered by the aerodynamic-lift control system and the divert-thrusters control system. By using game space decomposition, the parameter effects of divert-thrusters control system on homing performance are investigated. Under propellant limits and given the time constant of the divert-thrusters control system, the hit-to-kill performance requires the following conditions. Firstly, the maximum acceleration generated by the divert-thrusters control system is greater than a critical value. Secondly, the thrusters close after interception terminates. Thirdly, the operation time of the divert-thrusters control system is sufficient long to cancel the miss distance. These results are also demonstrated by a realistic ballistic missile-defense simulation program.

Suggested Citation

  • Yanfang Liu & Naiming Qi & Zhiwei Tang, 2013. "Effects of Divert-Thrusters on Homing Performance of Endo-atmospheric Interceptors," Journal of Optimization Theory and Applications, Springer, vol. 156(2), pages 345-364, February.
    • Handle: RePEc:spr:joptap:v:156:y:2013:i:2:d:10.1007_s10957-012-0119-1
    DOI: 10.1007/s10957-012-0119-1
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    References listed on IDEAS

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    1. T. Shima, 2005. "Capture Conditions in a Pursuit-Evasion Game between Players with Biproper Dynamics1," Journal of Optimization Theory and Applications, Springer, vol. 126(3), pages 503-528, September.
    2. V. Turetsky, 2004. "Upper Bounds of the Pursuer Control Based on a Linear-Quadratic Differential Game," Journal of Optimization Theory and Applications, Springer, vol. 121(1), pages 163-191, April.
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