远程空空导弹中制导策略的分析和评估  

Analysis and evaluation of midcourse guidance algorithm for long-range air-to-air missile

作　　者：王炀[1] 唐硕[1] 

机构地区：[1]西北工业大学航天学院,陕西西安710072

出　　处：《飞行力学》2012年第4期366-370,共5页Flight Dynamics

摘　　要：研究了远程空空导弹中制导策略的分析和评估问题。为了综合改善中制导策略在纵向和侧向平面内的飞行性能、提高评估结果的可信性和全面性,提出了一种基于最优控制理论的混合中制导策略,重点对中制导策略的飞行性能和作战性能两个方面进行了综合的评估。结果表明,所设计的中制导策略具有更广的射程范围和最大的攻击区、更短的飞行时间和更大的末端能量。This paper focuses on analysis and evaluation of midcourse guidance algorithm for long-range air-to-air missile.In order to improve flight performance in both horizontal and vertical planes and make the evaluation results more reliable and comprehensive,a hybrid midcourse guidance method based on optimal control theory is developed,and evaluated the proposed midcourse guidance method on two aspects of flight and combat performances is evaluated.The evaluation results show that the proposed midcourse guidance method is superior in attainable area,maximum attacking area,flight period and final energy.

关 键 词：远程空空导弹 中制导 分析 评估 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程]