Cooperative guidance of seeker-less missile with two leaders

Jianbo Zhao, Shuxing Yang*, Fenfen Xiong

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

19 Citations (Scopus)

Abstract

Based on the centralized leader-follower framework, a novel cooperative guidance strategy is proposed to implement the fire-and-forget attacks of seeker-less missiles in which the motion information of a maneuvering target and the strict requirement on the convergence time of the position are not required for the seeker-less missile. First, based on the motion states of two seeker-guided missiles, a virtual target (a point or line) that can certainly arrive at or cover the maneuvering target is carefully selected. Then, two cooperative guidance laws corresponding to the point and line virtual target are derived based on the consensus theory and dynamic inversion control, respectively. One of the guidance laws can implement the simultaneous attack of multiple missiles by employing both normal and tangential overloads, while the other is more practical to be employed as it only controls the normal overload of the seeker-less missile, even though the simultaneous attack cannot be implemented. Simulations are conducted, and the impact of the guidance parameters on the guidance performance is also studied. The results demonstrate the effectiveness of the proposed cooperative guidance laws.

Original languageEnglish
Pages (from-to)308-315
Number of pages8
JournalAerospace Science and Technology
Volume88
DOIs
Publication statusPublished - May 2019

Keywords

  • Consensus theory
  • Cooperative guidance
  • Dynamic inversion control
  • Fire-and-forget attack
  • Seeker-less missile
  • Virtual target

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