Time-varying sliding mode guidance scheme for maneuvering target interception with impact angle constraint

被引:29
作者
Ji, Haibo [1 ,2 ]
Liu, Xiangdong [1 ,2 ]
Song, Zhuoyue [1 ,2 ]
Zhao, Yao [3 ]
机构
[1] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
[2] Minist Educ Peoples Republ China, State Key Lab Intelligent Control & Decis Complex, Beijing 100081, Peoples R China
[3] China Acad Launch Vehicle Technol, Beijing 100076, Peoples R China
来源
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS | 2018年 / 355卷 / 18期
基金
中国国家自然科学基金;
关键词
LAW; SYSTEMS; DESIGN;
D O I
10.1016/j.jfranklin.2017.01.036
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, a guidance scheme for impact angle control against maneuvering targets with unknown target acceleration is proposed. In this scheme, the unknown target acceleration is estimated via a linear extended state observer; a novel time-varying global slide mode control technique is presented to eliminate the reaching phase and enforce a desired impact angle exactly at the time of interception with finite-time convergence, good robustness, high precision and smooth guidance command Moreover, feasible guidance logics are developed to achieve all-aspect interception with the tolerance of large initial heading errors. Numerical simulations in various scenarios are performed to verify the performance of the proposed guidance scheme. (C) 2017 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:9192 / 9208
页数:17
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