Multiple Angle Impact Guidance Law Design for Hypersonic Guided Rockets

被引：0

作者：

Li, Jinping ^{[1
]}

Mao, Zhaoyong ^{[2
]}

Li, Yajun ^{[1
]}

Chang, Guannan ^{[1
]}

机构：

[1] Xian Modern Control Technol Res Inst, Xian 710065, Peoples R China

[2] Northwestern Polytech Univ, Xian 710069, Peoples R China

来源：

PROCEEDINGS OF 2022 INTERNATIONAL CONFERENCE ON AUTONOMOUS UNMANNED SYSTEMS, ICAUS 2022 | 2023年 / 1010卷

关键词：

Hypersonic rockets; Multiple angle impact; Impact angle constraint; Implementation approach;

D O I：

10.1007/978-981-99-0479-2_123

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

To Guarantee the warhead effectiveness, it usually requires that the hypersonic guided rocket attacks the target with a designated and sufficient large impact angle. To address such problem, a new multiple angle impact guidance law is proposed in this paper. Firstly, the design process of the proposed guidance law with impact angle constraint is presented. Then, the implementation approach of the developed guidance law is analyzed. Finally, the correctness and validity of the guidance law are verified by the simulation of the closed-loop 6-dof model.

引用

页码：1349 / 1355

页数：7

共 50 条

[31] Integrated Guidance and Control Law with Impact Angle Constraint
Yun, Joongsup
Ryoo, Chang-Kyung
2011 11TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS (ICCAS), 2011, : 1239 - 1243
[32] A Nonlinear Suboptimal Guidance Law with Impact Angle Constraint
Guo Peng-fei
She Hao-ping
2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 4910 - 4914
[33] Optimal impact angle guidance law with barrier constraint
Jung, Cheol-Goo
Wang, Pengyu
Lee, Chang-Hun
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2024, 238 (11) : 1055 - 1067
[34] Design of H∞ Guidance Law with Terminal Angle Constraint
郭建国
周军
火力与指挥控制, 2009, (12) : 44 - 46
[35] Design of guidance law of missile in attack with high angle
Bao, Yiming
Jiang, Zhichao
Peng, Chen
Wu, Sentang
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2008, 34 (12): : 1375 - 1378
[36] Guidance law for hypersonic descent to a point
Eisler, G.Richard, 1600, Publ by AIAA, Washington, DC, United States (17):
[37] Optimal guidance law of satellite guided bombs with large landing angle
Dou, Lei
Yang, Xin-Min
Nanjing Li Gong Daxue Xuebao/Journal of Nanjing University of Science and Technology, 2010, 34 (03): : 314 - 318
[38] GUIDANCE LAW FOR HYPERSONIC DESCENT TO A POINT
EISLER, GR
HULL, DG
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1994, 17 (04) : 649 - 654
[39] Impact time control guidance law with large impact angle constraint
Zhang, Youan
Wang, Xingliang
Ma, Guoxin
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2015, 229 (11) : 2119 - 2131
[40] Nonsingular Terminal Sliding-Mode-Based Guidance Law Design with Impact Angle Constraints
Xiaojian Zhang
Mingyong Liu
Yang Li
Iranian Journal of Science and Technology, Transactions of Electrical Engineering, 2019, 43 : 47 - 54

← 1 2 3 4 5 →