Distributed target-encirclement guidance law for cooperative attack of multiple missiles

Author:

Yan Pengpeng1ORCID,Fan Yonghua1,Liu Ruifan12,Wang Mingang1

Affiliation:

1. School of Astronautics, Northwestern Polytechnical University, Xi’an, People’s Republic of China

2. Centre for Autonomous and Cyber-Physical Systems, Cranfield University, Cranfield, UK

Abstract

The target-encirclement guidance problem for many-to-one missile-target engagement scenario is studied, where the missiles evenly distribute on a target-centered circle during the homing guidance. The proposed distributed target-encirclement guidance law can achieve simultaneous attack of multiple missiles in different line-of-sight directions. Firstly, the decentralization protocols of desired line-of-sight angles are constructed based on the information of neighboring missiles. Secondly, a biased proportional navigation guidance law that can arbitrarily designate the impact angle is cited. The missiles can achieve all-aspect attack on the target in an encirclement manner by combining the biased proportional navigation guidance law and dynamic virtual targets strategy. Thirdly, the consensus protocol of simultaneous attack is designed, which can guarantee that all missiles’ time-to-go estimates achieve consensus asymptotically, and the convergence of the closed-loop system is proved strictly via the Lyapunov stability theory. Finally, numerical simulation results demonstrate the performance and feasibility of the proposed distributed target-encirclement guidance law in different engagement situations.

Funder

Aeronautical Science Foundation of China

Publisher

SAGE Publications

Subject

Artificial Intelligence,Computer Science Applications,Software

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