直升机载空空导弹机弹相容性仿真研究  

Study of Compatibility between Helicopter and Helicopter-borne AAM

作　　者：王维强[1] 任宏光[1] 崔颢[1,2] 白涛涛[1] 

机构地区：[1]中国空空导弹研究院,河南洛阳471009 [2]航空制导武器航空科技重点实验室,河南洛阳471009

出　　处：《弹箭与制导学报》2014年第1期37-40,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：直升机载空空导弹是武装直升机空战、夺取超低空制空权的主要武器装备,其与载机平台的相容性问题必须进行重点研究;通过建立导弹6自由度数学模型及导弹尾流场模型等,对空空导弹在直升机上发射离轨过程、初始弹道、发动机尾流场以及喷出物等全过程进行了仿真和分析,并给出了研究结论;同时为避免初始弹道的下沉带来的消极影响,对导弹初始弹道控制给出了建议。Helicopter-borne AAM is the primary weapon of the armed helicopter to control of the low-ahitude air. The compatibility between helicopter and helicopter-home AAM is required study as emphases. Established the 6-DOF model and the ejecta model of AMM. Simula- ted, computed ＆ researched the whole process of AAM launch from helicopter, it include movement on track,guise of slide away, initial trajectory,plume and ejecta. Through the study, found the conclusion that the compatibility between one type helicopter and the AMM is well. Another,in order to avoid going down of the initial trajectory, to table a proposal for the design of the thrust deflection.

关 键 词：直升机载空空导弹 机弹相容性 轨上运动 离轨姿态 初始弹道 尾流 喷出物 

分 类 号：TJ762.2[兵器科学与技术—武器系统与运用工程]