Volume 26 Issue 7
Jul.  2011
Turn off MathJax
Article Contents
QI Zhao-hui, LIANG Wei, LIU Xue-mei, ZHAI Li-li, GAO Lan. Optimization design of trajectory-control engine of interceptor based on zero-effort-miss[J]. Journal of Aerospace Power, 2011, 26(7): 1654-1658.
Citation: QI Zhao-hui, LIANG Wei, LIU Xue-mei, ZHAI Li-li, GAO Lan. Optimization design of trajectory-control engine of interceptor based on zero-effort-miss[J]. Journal of Aerospace Power, 2011, 26(7): 1654-1658.

Optimization design of trajectory-control engine of interceptor based on zero-effort-miss

  • Received Date: 2010-05-12
  • Rev Recd Date: 2011-01-23
  • Publish Date: 2011-07-28
  • To improve the transport and intercepting capability of interceptor considering the relative distance and velocity between target and interceptor, etc, the zero-effort-miss model of interceptor, the internal ballistic model and the mass & size model of trajectory-control engine were established to optimize the trajectory-control engine. The genetic arithmetic combined with Powell method was also adopted in the optimization design of trajectory-control engine. The zero-effort-miss eliminated by trajectory-control engine could improve not less than 17.9% as proved by the optimization design case, and the influence caused by uncertain factors was more explicit, so the method might be applied to the optimization design of interceptor.

     

  • loading
  • [1]
    刘世勇,吴瑞林,周伯昭.大气层外拦截器末段轨控发动机开关控制律[J].宇航学报,2005,26(10):106-109. LIU Shiyong,WU Ruilin,ZHOU Bozhao.An on-of control law of a divert thruster for an exoatmospheric interceptor during its terminal course[J].Journal of Astronautics,2005,26(10):106-109.(in Chinese)
    [2]
    张国舟.微推进系统的轨控发动机动态分析[J].北京航空航天大学学报,1999,25(6):688-691. ZHANG Guozhou.Transient analysis of a divert thruster for micropropulsion systems[J].Journal of Beijing University of Aeronautics and Astronautics,1999,25(6):688-691.(in Chinese)
    [3]
    Acampora K J,Wichmann H.Component development for micro-propulsion systems .AIAA 92-3255,1992.
    [4]
    孙中豪,陈新华.基于比例导航的轨控发动机动力装置参数分析[J].装备指挥技术学院学报,2006,17(4):52-55. SUN Zhonghao,CHEN Xinhua.Analysis of power parameter in trajectory controlling engine based on proportional navigation[J].Journal of the Academy of Equipment Command & Technology,2006,17(4):52-55.(in Chinese)
    [5]
    Chiang M J,Su Y P,Chang S D.The optimization of solid rocket vehicles .AIAA 83-1251,1983.
    [6]
    Anderson M,Burkhalter J,Jenkins R.Multi-disciplinary intelligent systems approach to solid rocket motor design Part Ⅰ:single and dual goal optimization .AIAA 2001-3599,2001.
    [7]
    Anderson M,Burkhalter J,Jenkins R.Multi-disciplinary intelligent systems approach to solid rocket motor design Part Ⅱ:multiple goal optimization .AIAA 2001-3600,2001.
    [8]
    吴启星,李晓斌,张为华.基于可信性理论的标准-3拦截弹末段修正能力分析[J].国防科技大学学报,2007,29(4):37-41. WU Qixing,LI Xiaobin,ZHANG Weihua.Creditability theory-based analysis for terminal divert ability of Standard Missile-3[J].Journal of National University of Defense Technology,2007,29(4):37-41.(in Chinese)
    [9]
    Sforzini R H.The optimization of solid rocket motor .AIAA 81-115,1981.
    [10]
    Anderson M,Burkhalter J,Jenkins R.Multi-disciplinary intelligent systems approach to solid rocket motor design Part Ⅱ:multiple goal optimization .AIAA 2001-3600,2001.
    [11]
    Salajegheh E,Gholizadeh S.Optimum design of structures by an improved genetic algorithm using neural networks[J].Advances in Engineering Software,2005,36(11-12):757-767.
    [12]
    李晓斌,张为华,王中伟.固体火箭发动机装药不确定性优化设计[J].固体火箭技术,2006,29(4):269-273. LI Xiaobin,ZHANG Weihua,WANG Zhongwei.Uncertainty optimization design of solid rocket motor grain[J].Journal of Solid Rocket Technology,2006,29(4):269-273.(in Chinese)
  • 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 (1779) PDF downloads(14) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return