Research on the Guidance Law for Spiral Maneuver of Air-to-ship Missile in Dive Trajectory Phase

SONG Gui-bao;ZHU Ping-yun;LI Hong-liang

CN Submission Journal Articles Figures Search
Adv. Search

  • Sponsored by: China Association for Science and Technology (CAST)

    Editor-In-Chief: Xu Yida

    ISSN 1000-1093

    　

  • Hosted By: China Ordnance Society

    Published By: Acta Armamentarii

    CN 11-2176/TJ

Acta Armamentarii, a Chinese monthly journal, was first published in 1979. The journal is supervised by China Association for Science and Technology, sponsored by China Ordnance Society，and edited and published by Editorial Board of Acta Armamentarii. The Journal is included in all important domestic databases，and also collected by Engineering Index (EI, USA), Chemical Abstracts (CA, USA), Science Abstracts (SA, UK）, Abstract Journal (AJ, Russia), and Current Bibliography on Science and Technology(CBST).Acta Armamentarii has been selected into the journal Of Ordnance Science and Technology (Weapons Industry) Field Of High Quality Scientific and Technological Periodical Classification Catalogue (2022 edition), ranking T1, and the journal of Automotive Engineering Field of High Quality Scientific and technological Periodical classification Catalogue, ranking T2.
Acta Armamentarii ›› 2014, Vol. 35 ›› Issue (2) : 220-227. DOI: 10.3969/j.issn.1000-1093.2014.02.013
Paper

Research on the Guidance Law for Spiral Maneuver of Air-to-ship Missile in Dive Trajectory Phase

  • SONG Gui-bao1, ZHU Ping-yun2, LI Hong-liang3
Author information +
History +

Abstract

For the penetration probability of air-to-ship missile adopting traditional flight trajectory is poor when it is intercepted by long-range ship-to-air missile, a scheme of modifying the descending phase trajectory to spiral maneuver dive trajectory is proposed. The design process of variable structure guidance law with terminal angular constraint is analyzed. On this basis, a kind of spiral maneuver variable structure guidance law is proposed. It can be used to guide the air-to-ship missile to realize the spiral maneuver dive trajectory, and ensure that the air-to-ship missile turns into the low altitude cruise phase in the end of the descending phase. The simulation results show that the proposed spiral maneuver variable structure guidance law improves remarkably the penetration probability of air-to-ship missile against the long-range ship-to-air missile.

Key words

control science and technology / air-to-ship missile / large airspace flight trajectory / spiral maneuver / variable structure guidance law

Cite this article

EndNote

Ris (Procite)

Bibtex

Download Citations
SONG Gui-bao, ZHU Ping-yun, LI Hong-liang. Research on the Guidance Law for Spiral Maneuver of Air-to-ship Missile in Dive Trajectory Phase. Acta Armamentarii. 2014, 35(2): 220-227 https://doi.org/10.3969/j.issn.1000-1093.2014.02.013

References

［1］ 顾文锦，赵红超. 基于虚拟目标的反舰导弹的最优制导律研究[J]. 现代防御技术, 2006, 34（4）:56-60.
GU Wen-jin, ZHAO Hong-chao. Research on the optimal guidance law for anti-ship missile based on the virtual targets[J]. Modern Defense Technology, 2006,34（4）:56-60.（in Chinese）
［2］ 赵红超, 王凤莲, 顾文锦. 带落角约束的反舰导弹变结构中制导律研究[J]. 战术导弹控制技术, 2006 （1）:20-22.
ZHAO Hong-chao, WANG Feng-lian, GU Wen-jin. Variable structure midcourse guidance law with angle constraint for anti-ship[J]. Control Technology of Tactical Missile, 2006（1）:20-22.（in Chinese）
［3］ 毕兰金, 张国庆, 顾文锦. 变结构制导律在大空域变轨反舰导弹弹道中的应用[J]. 战术导弹技术, 2010（2）:73-76.
BI Lan-jin, ZHANG Guo-qing, GU Wen-jin. An application of variable structure guidance law to large-space variable trajectory of anti-ship missile[J]. Tactical Missile Technology, 2010（2）:73-76.（in Chinese）
［4］ ShinarJ, Tabak R. New results in optimal missile avoidance analysis [J]. Journal of Guidance, Control, and Dynamics, 1994, 17（5）:897-902.
［5］ OhlmeyerE J. Root-mean-square miss distance of proportional navigation missile against sinusoidal target[J]. Journal of Guidance, Control and Dynamics, 1996, 19（3）: 563-568.
［6］ 姜玉宪,崔静. 导弹摆动式突防策略的有效性[J].北京航空航天大学学报, 2002, 28（2）:133-136.
JIANG Yu-xian, CUI Jing. Effectiveness of weaving maneuver strategy of a missle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002,28（2）:133-136.（in Chinese）
［7］ 顾文锦，赵红超，王凤莲. 反舰导弹末端机动的突防效果研究[J]. 宇航学报, 2005, 26（6）:758-761.
GU Wen-jin, ZHAO Hong-chao, WANG Feng-lian. Research on the penetration effect of terminal maneuver for anti-ship missiles[J]. 2005, 26（6）:758-761.（in Chinese）
［8］ 周荻，邹昕光，孙德波. 导弹机动突防滑模制导律[J]. 宇航学报, 2006, 27（2）:213-216.
ZHOU Di, ZOU Xin-guang, SUN De-bo. A sliding-mode guidance law for homing-missiles breaking through defense with maneuver[J]. Journal of Astronautics, 2006, 27（2）: 213-216.（in Chinese）
［9］ 张汝川, 顾文锦, 赵红超. 基于主动螺旋变轨的三维末制导律研究[J]. 兵工学报, 2009, 30（6）:720-726.
ZHANG Ru-chuan, GU Wen-jin, ZHAO Hong-chao. Research on 3D terminal guidance laws based on actively self-homing spiral variable trajectory[J]. Acta Armamentarii, 2009, 30（6）:720-726.（in Chinese）
［10］ 范作娥. 带落角约束的反舰导弹末端导引与机动研究[D]. 烟台：海军航空工程学院，2010:86-105.
FAN Zuo-e. Research on the terminal guidance and maneuvering with angle constraint for anti-ship[D]. Yantai: Naval Aeronautical Engineering Institute，2010:86-105. (in Chinese)
［11］ ZhouD, Mu C, Xu W. Adaptivesliding-mode guidance of a homing missile[J]. Journal of Guidance, Control and Dynamics, 1999, 22（4）: 589-594.

Collection(s)

Guidance

Ballistics

622

Accesses

0

Citation

Detail
Sections
Recommended

/

〈 〉