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
  • [41] ASSESS THE ABILITY TO INTERCEPT CRUISE MISSILES OF SURFACE-TO-AIR MISSILE SYSTEM
    Hong, Nguyen Minh
    AD ALTA-JOURNAL OF INTERDISCIPLINARY RESEARCH, 2019, 9 (01): : 139 - 145
  • [42] Conceptual form of information subsystem of antiaircraft guided missile of promising AMS
    Avlasyonok A.V.
    Alekseev E.G.
    Litvinov S.P.
    Savitskii F.L.
    Radioelectronics and Communications Systems, 2008, Allerton Press Inc. (51) : 267 - 270
  • [43] Intercept debris safety analysis and avoidance screening for ballistic missile intercept testing
    Mule, JN
    McKnight, D
    CHARACTERISTICS AND CONSEQUENCES OF ORBITAL DEBRIS AND NATURAL SPACE IMPACTORS, 1996, 2813 : 2 - 15
  • [44] Modeling of Calculation Error Series of Antiaircraft Gun Weapon Systems
    Tao De-jin
    Bo Yu-ming
    Wang Jun
    2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 8497 - 8500
  • [45] EVERY GUN A MISSILE LAUNCHER
    DEMEIS, R
    AEROSPACE AMERICA, 1985, 23 (06) : 44 - &
  • [46] Navy's missile defense closes in on intercept
    Wall, R
    Nordwall, BD
    AVIATION WEEK & SPACE TECHNOLOGY, 2001, 154 (06): : 39 - 39
  • [47] Effects of towed-decoys against antiaircraft missile with monopulse seeker
    Gao B.
    Mao S.-Y.
    Sun J.-P.
    Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics, 2010, 32 (11): : 2394 - 2397
  • [48] Demonstration of a precision missile intercept measurement technique
    Thompson, T
    JOHNS HOPKINS APL TECHNICAL DIGEST, 1998, 19 (04): : 513 - 523
  • [49] Missile Guidance With Constrained Intercept Body Angle
    Rusnak, Ilan
    Weiss, Haim
    Eliav, Rei
    Shima, Tal
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2014, 50 (02) : 1445 - 1453
  • [50] MISSILE SIZING FOR ASCENT-PHASE INTERCEPT
    HULL, DG
    SALGUERO, DE
    JOURNAL OF SPACECRAFT AND ROCKETS, 1995, 32 (03) : 445 - 449