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Journal of Projectiles, Rockets, Missiles and Guidance >

2015 , Vol. 35 >Issue 5: 149 - 154

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2015.05.035

CORRELATION TECHNOLOGY

Research on Cooperative Multiple-missile Intercepting Strategy for Near-space Vehicles

  • HUI Yaoluo ,
  • NAN Ying ,
  • CHEN Shaodong ,
  • YANG Yi
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  • 1 College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
    2 Science and Technology on Electro-optic Control Laboratory, Henan Luoyang 471009, China

Received date: 2014-10-31

  Online published: 2025-05-28

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Abstract

This paper provides an effective intercepting strategy for mission intercepting near-space vehicles using multi-to-multi confrontation. Concrete research was constitutive of the following two parts: firstly, intercepting tasks were allocated to flight vehicles based on genetic algorithm to optimize efficiency of intercepting system. Secondly, the 4-D impact time control guidance law (ITCG) was designed in forepart of interception based on theory of sliding mode control for basically identical intercepting time. Pure PNG law was adopted in terminal maneuvering ballistic trajectory to ensure that cooperative interception was accurate. Numerical simulation results show that this intercepting strategy can achieve highly reliable and accurate interception for multiple missiles intercepting multiple hypersonic near-space vehicles.

Key words： dynamic task allocation; impact time control guidance; genetic algorithm; sliding mode control theory; near-space vehicle; flight numerical simulation

Cite this article

HUI Yaoluo , NAN Ying , CHEN Shaodong , YANG Yi . Research on Cooperative Multiple-missile Intercepting Strategy for Near-space Vehicles[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(5) : 149 -154 . DOI: 10.15892/j.cnki.djzdxb.2015.05.035

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