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双拦截弹拦截单目标边界型微分对策制导律研究
作者姓名:张帅  朱东方  孙俊  华春  刘延芳
作者单位:航空工业哈尔滨飞机工业集团有限责任公司,上海航天控制技术研究所上海,上海航天控制技术研究所上海,上海航天信息研究所,哈尔滨工业大学 航天学院
基金项目:SAST基金(SAST-2018-109)、上海科技人才计划项目(16XD1421000)
摘    要:针对战术弹道导弹、高超声速巡航导弹和无人飞行器等新型具有高机动性能的防空目标,为提高成功拦截的概率,采用多枚拦截弹进行拦截。应用微分对策理论,将双拦截弹拦截单目标的末段制导问题建模为“二对一追踪-逃逸”对策模型。考虑最大加速度约束,研究了两枚拦截弹的拦截空间分解和对策空间分布,并通过仿真研究了制导律性能。结果表明:采用两枚拦截弹拦截时,脱靶量对目标机动方向的转变时间具有很好的鲁棒性。

关 键 词:边界型微分对策  拦截  二对一追踪-逃逸  拦截空间  制导
收稿时间:2019/2/21 0:00:00
修稿时间:2019/3/12 0:00:00

Bounded Differential Games Strategies with Two-Pursuit Single-Evader
Authors:ZHANG Shuai  ZHU Dongfang  SUN Jun  Hua Chun and LIU Yanfang
Institution:AVIC Harbin Aircraft Industry Group CoLTD,Shanghai Institute of Spaceflight Control Technology,Shanghai Institute of Spaceflight Control Technology,Space information Institute,School of Astronautics,Harbin Institute of Technology
Abstract:In order to intercept the future target such as tactical ballistic missile (TBM) and supersonic cruise missile (SCM) and unmanned aerial vehicle (UAV) witch are characterized by high maneuvering capability, multiple interceptors may be launched and aimed at single target. The end-game guidance of intercepting single target with two missiles is modeled as a two-pursuit single-evader game model and solved by bounded differential game theory. The intercept space decomposition and game space structure are investigated and homing performance are demonstrated by simulations of a realistic ballistic missile defense scenario. Results show that: the miss distance has robust performance with respect to the maneuvering direction changing time by utilizing two interceptors.
Keywords:bounded differential games  interception  two-pursuit single-evader  intercept space  guidance
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