Cooperative Guidance of Seeker-Less Missiles for Precise Hit

Author:

Zhao Jianbo1ORCID,Xiong Fenfen1ORCID

Affiliation:

1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Abstract

A novel cooperative guidance scenario is proposed that implements fire-and-forget attacks for seeker-less missiles with a cheap finder for stationary targets and without requiring real-time communication among missiles or precise position information. Within the proposed cooperative scenario, the classic leader-follower framework is utilized, and a two-stage cooperative guidance law is derived for the seeker-less missile. Linear-quadratic optimal control and biased proportional navigation guidance (PNG) are employed to develop this two-stage cooperative guidance law to minimize the control cost in the first stage and to reduce the maximum acceleration command in the second stage when the acceleration command is continuous. Simulations and comparisons are conducted that demonstrate the effectiveness and advantages of the proposed guidance law.

Funder

Hongjian Innovation Foundation of China

Publisher

Hindawi Limited

Subject

Aerospace Engineering

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Distributed observer‐based fixed‐time cooperative guidance law against maneuvering target;International Journal of Robust and Nonlinear Control;2023-08-29

2. An Analysis Method for Hit Accuracy of Gun-Launched Reconnaissance and Strike Integrated Unmanned Aerial Vehicle;2022 IEEE 2nd International Conference on Information Communication and Software Engineering (ICICSE);2022-03-18

3. Distributed observer-based cooperative guidance with appointed impact time and collision avoidance;Journal of the Franklin Institute;2021-09

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