一种新型的直升机载空地导弹中制导规律通用设计方法  

A New Type of General Design Method for Median Guidance Law in Air-to-ground Missile Carried by Helicopter

作　　者：马菲 杨凯 王妮芝 王荔豪 许琛 MA Fei;YANG Kai;WANG Nizhi;WANG Lihao;XU Chen(Xi'an Modem Control Technology Research Institute,Xi'an 710065,China)

机构地区：[1]西安现代控制技术研究所,西安710065

出　　处：《弹箭与制导学报》2019年第5期95-98,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：针对空地导弹不同发射高度、不同作战距离、不同导引头捕获域及擦地角约束条件及不同攻击模式对落角的各方面要求,提出了一种新型的空地导弹中制导规律通用设计方法,以同时满足多方面约束条件,并通过数学仿真验证了此方法的合理性和有效性。In view of the different launch altitude, different combat distance, different seeker’s capture field and the requirements of different attack modes of air-to-ground guided missiles, a new general design method of median guidance law is proposed to meet the various constraints at the same time in this paper.Mathematical simulation is adopted to verify the rationality and validity of the method.

关 键 词：空地导弹 中制导规律 数学仿真 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]