A modified cooperative proportional navigation guidance law

被引：51

作者：

Chen, Yadong ^{[1
]}

Wang, Jianan ^{[1
]}

Wang, Chunyan ^{[1
]}

Shan, Jiayuan ^{[1
]}

Xin, Ming ^{[2
]}

机构：

[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China

[2] Univ Missouri, Dept Mech & Aerosp Engn, Columbia, MO 65211 USA

来源：

JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS | 2019年 / 356卷 / 11期

基金：

中国国家自然科学基金;

关键词：

IMPACT-TIME; ATTACK;

D O I：

10.1016/j.jfranklin.2019.04.013

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 Jeon et al. (2010), a cooperative PNG (Proportional Navigation Guidance) law was proposed to achieve the salvo attack using multiple missiles. When the leading angle is near zero, singularity would occur, and the cooperation may fail. In this paper, a modified cooperative guidance law is presented to avoid such singularity existing in the guidance law in Jeon et al. (2010). The time-to-go control efficiency under small leading angle is also improved in this paper. The convergence of times-to-go to the same value using the proposed guidance law is guaranteed by the Lyapunov stability analysis. Simulation results show the effectiveness of the modified guidance law and the improved performance. (C) 2019 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.

引用

页码：5692 / 5705

页数：14

共 22 条

[1]

[Anonymous], 2011, IFAC P VOLUMES

[2]

Cho N., 2016, J GUID CONTROL DYNAM, V39, P1

[3] Accurate Time-to-Go Estimation for Proportional Navigation Guidance [J].

Dhananjay, N. ;

Ghose, D. .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2014, 37 (04) :1378-1383

[4]

Erer K. S., 2016, J GUID CONTROL DYNAM, V39, P1

[5] Impact Time and Angle Guidance With Sliding Mode Control [J].

Harl, Nathan ;

Balakrishnan, S. N. .

IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2012, 20 (06) :1436-1449

[6]

He S., 2017, IEEE T AERO ELEC SYS, V54, P1555

[7]

Hull D. G., 2012, J GUID CONTROL DYNAM, V14, P865

[8] Homing Guidance Law for Cooperative Attack of Multiple Missiles [J].

Jeon, In-Soo ;

Lee, Jin-Ik ;

Tahk, Min-Jea .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (01) :275-280

[9] Impact-time-control guidance law for anti-ship missiles [J].

Jeon, IS ;

Lee, JI ;

Tahk, MJ .

IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2006, 14 (02) :260-266

[10] Time-varying sliding mode guidance scheme for maneuvering target interception with impact angle constraint [J].

Ji, Haibo ;

Liu, Xiangdong ;

Song, Zhuoyue ;

Zhao, Yao .

JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2018, 355 (18) :9192-9208

← 1 2 3 →