多机空战协同制导决策方法  

Decision methods for cooperative guidance in multi-aircraft air warfare

作　　者：肖冰松[1] 方洋旺[1] 胡诗国[1] 曾宪伟[1] 

机构地区：[1]空军工程大学工程学院,陕西西安710038

出　　处：《系统工程与电子技术》2009年第3期610-612,共3页Systems Engineering and Electronics

基　　金：国家自然科学基金(60674031);国家"863"高技术发展计划基金(2006AA701307);总装预研重点基金(6140529)资助课题

摘　　要：针对多机协同空战中需要将对中距空空导弹的中制导权移交给其他飞机的问题,提出制导优势的概念,用来表征编队内其他飞机对导弹协同制导的能力,从而为选择对导弹实施中制导的新平台提供辅助决策。在综合参战飞机双方角度、距离和速度等几何态势和飞机空战性能的基础上,探讨制导优势的计算方法。给出两种制导切换方式,分析了各自的优缺点。通过仿真实验,证明所提方法的可行性和有效性。To investigate the handover of guidance power for intermediate range air-to-air missile to other fighters in multi-aircraft cooperative air warfare, a new concept named guidance superiority is proposed. It is in token of the cooperative guidance ability of fighters in the formation, so as to provide assistant decision making of selecting a new guidance platform for the missile. The calculation method of guidance superiority is discussed, based on synthesizing the situation （including angle, distance and velocity） and the fighter capability of both sides in the warfare. Two modes of guidance switch are given. The virtue and the flaw are analyzed for each mode. The feasibility and the validity of the method are validated by the application example.

关 键 词：协同空战 协同制导 制导优势 制导切换 

分 类 号：V271.4[航空宇航科学与技术—飞行器设计] E926[军事—军事装备学]