首页 | 本学科首页   官方微博 | 高级检索  
     检索      

拦截机动目标的运动伪装制导律
引用本文:高长生,李涧青,荆武兴.拦截机动目标的运动伪装制导律[J].宇航学报,2016,37(6):737-743.
作者姓名:高长生  李涧青  荆武兴
作者单位:哈尔滨工业大学航天工程系,哈尔滨150001
基金项目:国家自然科学基金(11572097);航天科技集团联合创新基金(CASCHIT131C03)
摘    要:设计了一种基于运动伪装策略的拦截制导律。首先根据弹目相对位置关系得出双二阶动力学模型,依据运动伪装策略的运动特性给出导弹拦截目标的条件。然后利用此条件并结合弹目相对运动关系推导三维空间下的制导律。在推导过程中发现,原来的三维制导律设计可以简化为二维平面内设计,从而降低了设计难度。通过加入对目标机动的估计,给出一种适用于三维空间拦截的二维导引律。最后对该制导律进行仿真校验,并与纯比例导引律进行仿真对比,仿真结果表明所设计的制导律满足制导精度的需求。

关 键 词:导弹拦截  制导律  运动伪装  降维设计  
收稿时间:2015-07-16

Motion Camouflage Strategy Guidance Law for Intercepting Maneuvering Target
GAO Chang sheng,LI Jian qing,JING Wu xing.Motion Camouflage Strategy Guidance Law for Intercepting Maneuvering Target[J].Journal of Astronautics,2016,37(6):737-743.
Authors:GAO Chang sheng  LI Jian qing  JING Wu xing
Institution:Department of Aerospace Engineering, Harbin Institute of Technology, Harbin 150001,China
Abstract:An intercept guidance law based on motion camouflage strategy is proposed in this paper. According to the relative position between a missile and a target, the dual second order dynamics model is derived, and the missile interception conditions are given based on this model and the characteristics of the motion camouflage strategy. Then, the three-dimensional guidance law is derived by using the interception conditions and the motion relation of the missile and the target. In the process of derivation, the three-dimensional guidance law can be designed in a two-dimensional plane and the difficulty of guidance law design is reduced. A two-dimensional guidance law for three-dimensional space is derived by introducing the estimation for target maneuver. Finally, the interception simulation for the proposed guidance law is taken and compared with pure proportional guidance. The simulation results demonstrate the accuracy and the effectiveness of the proposed guidance law.
Keywords:Missile intercept  Guidance law  Motion camouflage  Dimension-reduction design  
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航学报》浏览原始摘要信息
点击此处可从《宇航学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号