Target Handover Between Midcourse and Terminal Guidance of Ship-Ship Cooperative Guidance for the Ship-Air Missile

被引:0
|
作者
Zhao Y. [1 ]
Jiao G. [1 ]
Wang J. [1 ]
Li Y. [1 ]
机构
[1] Naval Research Institute, Beijing
关键词
cooperative guidance; error model; interception probability; predetermined pointing angle; ship-air missile; target handover;
D O I
10.15918/j.tbit1001-0645.2021.212
中图分类号
学科分类号
摘要
Aiming at the target handover between the midcourse and terminal guidance in the process of ship-air missile intercepting target over the horizon guided by ship-ship cooperative guidance, a constraint condition was proposed for successful target handover. Firstly, projecting the missile-target line of sight angle vector to a corresponding rotation plane, a calculation model was established for the predetermined pointing angle of the seeker antenna to be suitable for the case of large predetermined pointing angle. And then, an error model was established based on variance analysis method for the predetermined pointing angle of the seeker antenna, and the error sources were analyzed combined with the cooperative guidance operation information flow. Finally, applying probability theory and permutation combination method, a success probability model of single target handover and multiple target handover were established. The simulation results verify the correctness of the predetermined pointing angle calculation error model and the target handover success probability model, as well as its effectiveness in reducing the predetermined pointing angle error and improving the target handover success probability. © 2022 Beijing Institute of Technology. All rights reserved.
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页码:953 / 960
页数:7
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共 15 条
  • [1] TENG Kenan, XIE Kongshu, PENG Fei, Design method for networked ship-to-air missile beyond line of sight cooperative anti-missile equipment architecture[J], Command Control & Simulation, 38, 2, pp. 89-95, (2016)
  • [2] TENG Kenan, Design Key Technalogies of networked ship-to-air missile beyond-visual-range cooperative anti-missile system[J], Electronics Optics & Control, 19, 12, pp. 1-5, (2012)
  • [3] WANG Guotian, WANG Hangyu, SHI Zhangsong, Analysis of coopetative guidance technology of us navy shio-to-air missile and its capability[J], Aerospace Shanghai, 29, 2, pp. 28-30, (2012)
  • [4] HU Yunan, ZHAO Yongtao, Design of the guidance law for ship-air missile beyond visual range and the instruction solution[J], Journal of Ballistics, 23, 1, pp. 88-92, (2011)
  • [5] ZHAO Yongtao, HU Yunan, CHEN Yu, Solution of antenna pointing angle of seeker for over-the-horizon ship-to-air missile[J], Systems Engineering and Electronics, 34, 11, pp. 24-28, (2012)
  • [6] ZHAO Y T, HU Y A., Research on the handover of the compound guidance for the anti-air missile beyond visual range[C], Proceedings of ICCIC 2011, pp. 224-231, (2011)
  • [7] ZHAO Shanyou, Design of the homing guidance and control system for the anti-air weapons, (2005)
  • [8] WANG Jun, LU Fugang, Study on pointing error of seeker[J], Acta Armamentarii, 30, 3, pp. 329-332, (2009)
  • [9] ZHOU Jin, WANG Huaji, ZHAO Wei, Suboptimal midcourse trajectory modification for hypersonic target interception[J], Transactions of Beijing Institute of Technology, 39, 8, pp. 839-845, (2019)
  • [10] LI Jia, Study of the target acquisition probability of composite guided middle/long range air-to-air missile, (2016)