Volume 28 Issue 2
Feb.  2002
Turn off MathJax
Article Contents
JIANG Yu-xian, CUI Jing. Effectiveness of Weaving Maneuver Strategy of a Missile[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(2): 133-136. (in Chinese)
Citation: JIANG Yu-xian, CUI Jing. Effectiveness of Weaving Maneuver Strategy of a Missile[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(2): 133-136. (in Chinese)

Effectiveness of Weaving Maneuver Strategy of a Missile

  • Received Date: 19 Jun 2000
  • Publish Date: 28 Feb 2002
  • Effectiveness of weaving maneuver strategy of a missile when it passes through a Missile-Defence-System(MDS) is addressed. A linearized planar engagement model is used. Closed form solutions for the miss distance of interceptor are derived from the case where the interceptor's guidance system is modeled by a first-order lag and the maneuver acceleration is unlimited. The miss solutions consist of two components, one is the transient, the other is the steady. The effectiveness is measured in terms of the break-defence probability over a set of engagements in which the weaving-durations are normally distributed around its desired value. Comparisons are made between the effectiveness of the transient and the steady weaving maneuver strategy .

     

  • loading
  • [1]玉宪.弹道导弹末制导段的规避控制. 见:全国第八届空间及运动体控制技术学术会议论文集. 北京:航空学会,1998.88~93. [2]姜玉宪.具有规避能力的末制导方法. 见:中国航空学会控制与应用第八届学术年会论文集. 北京:航空学会,1998.75~79. [3]Zarchan P. Proportional navigation and weaving targets[J].Journal of Guidance Control and Dynamics,1995,18(5):969~974. [4]Ohlmeyer E 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. [5]Takehira T.Analytical solution of missile terminal guidance [J].Journal of Guidance Control and Dynamics,1998,21(2):342~348. [6]Shinar J, Steinberg D. Analysis of optimal evasive maneuvers based on a linearized two-dimension kinematics model[J].Journal of Aircraft, 1977,14(8):795~801. [7]Forte I, Shinar J. Can a mixed guidance strategy improve missile performance [J].Journal of Aircraft, 1988,11(1):53~58. [8]Nesline F W, Zarchen P. A new look at classical vs modern homing missile guidance [J].Journal of Guidance and Control ,1981,4(1):78~85. [9]姜玉宪.控制系统仿真[M]. 北京:北京航空航天大学出版社,1998.105~115. [10]archan P. Tactical and strategic missile guidance[M]. Washington DC:AIAA Inc,1990.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views(2559) PDF downloads(889) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return