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[an error occurred while processing this directive]基于动态逆的多弹协同作战三维制导律研究
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马泽远(1995—),男,辽宁鞍山人,硕士研究生,研究方向:飞行器总体设计。 |
收稿日期: 2020-05-10
网络出版日期: 2025-02-20
Research on Three-dimensional Guidance Law for Cooperative Attack of Multiple Missiles Based on Dynamic Inversion
Received date: 2020-05-10
Online published: 2025-02-20
马泽远 , 卢宝刚 , 李墨吟 , 李威 , 夏群利 . 基于动态逆的多弹协同作战三维制导律研究[J]. 弹箭与制导学报, 2021 , 41(3) : 43 -47 . DOI: 10.15892/j.cnki.djzdxb.2021.03.010
In order to achieve cooperative saturation attack of multi-missiles on the same target, the nonlinear relative motion model is designed based on the relative motion relationship between the missile and the target, and a multi-missile time coordination three-dimensional guidance law is proposed based on the leader-follower cooperative guidance model. In the guidance law, the leader missile adopts three-dimensional pure proportional navigation guidance, and follower missiles use three-dimensional pure proportional navigation guidance and dynamic inverse control. To achieve the consistent impact time, the follower nonlinear model is divided into a fast subsystem and a slow subsystem according to the time-scale separation method, and then feedback linearization of two subsystems is achieved based on dynamic inverse system theory to complete the cooperative control of the follower. Simulation results show that the use of this cooperative guidance rate can enable the missiles to hit the target at the same time, effectively achieving the coordination of attack time.
Key words: missile; dynamic inversion; cooperative guidance; impact time
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