Simulation system of antiaircraft gun to intercept cruising missile

被引:0
|
作者
Mou, Da-Wei [1 ]
Cai, Tao [1 ]
Dou, Li-Hua [1 ]
机构
[1] Dept. of Automat. Control, Sch. of Info. Sci. and Technol., Beijing Inst. of Technol., Beijing 100081, China
关键词
Computer simulation - Database systems - Missiles - Targets;
D O I
暂无
中图分类号
学科分类号
摘要
The tactical assumption of antiaircraft gun system to intercept cruising missile is researched by digital simulation. The problem of target creation is discussed. Then the antiaircraft gun system including fire control system, tracking system, shootable zone and external trajectory is described. After establishing simulation database, the forward relevant software design project is presented. The simulation system can be used to evaluate the effect of intercept missile by single gun, and integrate with other simulation system.
引用
收藏
页码:39 / 43
相关论文
共 50 条
  • [21] Design of built-in-test system in a certain type of antiaircraft missile weapon system
    Zhou, MJ
    Chen, JH
    Lin, HT
    Gao, FQ
    ISTM/2005: 6th International Symposium on Test and Measurement, Vols 1-9, Conference Proceedings, 2005, : 8685 - 8687
  • [22] The scene simulation of antiaircraft weapon servo system
    Yang, ZB
    Zhu, YC
    Fan, SY
    Dong, ST
    ISTM/2001: 4TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1 AND 2, CONFERENCE PROCEEDINGS, 2001, : 757 - 760
  • [23] A fault diagnostic expert system design of antiaircraft missile based on fuzzy logic
    Liu, M
    Zhang, JW
    Ren, BX
    ICEMI'2003: PROCEEDINGS OF THE SIXTH INTERNATIONAL CONFERENCE ON ELECTRONIC MEASUREMENT & INSTRUMENTS, VOLS 1-3, 2003, : 941 - 944
  • [24] Design of virtual test mode on the antiaircraft gun weapon system firing test
    Yang, Lin
    Meng, Xianguo
    Zhu, Yuanchang
    Di, Yanqiang
    PROCEEDINGS OF THE 2012 SECOND INTERNATIONAL CONFERENCE ON INSTRUMENTATION & MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC 2012), 2012, : 383 - 385
  • [26] Determination of antiaircraft missile's optimal testing cycle
    Liu, M
    Gao, KH
    Yu, JM
    ISTM/2005: 6th International Symposium on Test and Measurement, Vols 1-9, Conference Proceedings, 2005, : 9087 - 9088
  • [27] Study on Inefficient Factors and Storage Reliability for the Antiaircraft Missile
    Li Ke
    Li Yan
    Jiang Huixia
    Zhang Kai
    PROCEEDINGS OF THE 2016 4TH INTERNATIONAL CONFERENCE ON MACHINERY, MATERIALS AND COMPUTING TECHNOLOGY, 2016, 60 : 1465 - 1470
  • [28] Rigid-flex coupled modeling and simulation of a super-light antiaircraft machine gun
    Fan, Lei
    Wang, Ya-Ping
    Liu, Yi-Ming
    Xu, Cheng
    Dandao Xuebao/Journal of Ballistics, 2009, 21 (01): : 67 - 70
  • [29] Study on Evaluation Subsystem of Tactical Antiaircraft Missile Hardware-In-Loop Simulating System
    Li Ke
    Liu Peng
    Zheng Silong
    ISTM/2011: 9TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, 2011, : 808 - 811
  • [30] Complementation of archibald and antiaircraft missile in low range air and anti-missile defence
    Bo, Yuming
    Guo, Zhi
    Du, Guoping
    Yang, Shaoyu
    Binggong Xuebao/Acta Armamentarii, 2002, 23 (02):