Prescribed-time guidance scheme design for missile salvo attack

被引:11
作者
Cui, Lei [1 ]
Jin, Nan [2 ]
Chang, Shaoping [1 ]
Zuo, Zhiqiang [1 ]
机构
[1] Tianjin Univ, Sch Elect & Informat Engn, Tianjin 300072, Peoples R China
[2] CASIC Res Inst Intelligent Decis Engn, Beijing 100074, Peoples R China
来源
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS | 2022年 / 359卷 / 13期
基金
中国国家自然科学基金;
关键词
SLIDING-MODE GUIDANCE; DISTURBANCE REJECTION; COOPERATIVE GUIDANCE; NONLINEAR-SYSTEMS; VARYING FEEDBACK; LAW; STABILIZATION; CONSENSUS;
D O I
10.1016/j.jfranklin.2022.07.008
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, for three-dimensional interception of multiple missiles on a maneuvering target, a prescribed-time salvo attack guidance scheme with impact angle constraints and impact time constraint is investigated. The target accelerations are estimated accurately by a prescribed-time extended state observer. With the proposed guidance scheme, it ensures the LOS angles converge to desired values within a predetermined convergence time, and achieves salvo attack at a predetermined impact time. Prescribed-time convergency is shown for the proposed observer and controllers. Finally, the validity of the proposed guidance scheme is verified through numerical simulation. (c) 2022 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:6759 / 6782
页数:24
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