摘要
为保证空空导弹试验靶场安全,并且有利于数据采集与事后分析,适应空空导弹回收控制新需求。文中考虑空空导弹体积限制,提出了一种无伞回收控制方法,仅依靠算法设计实现了导弹平稳回收。首先对回收需求进行分析,设计了回收控制启动判据,并提出基于航迹与姿态联合控制的回收算法。最后,通过具体实例验证了回收控制方法可行,算法执行效果良好,易于工程实现。
A new recovery method was applied for the air-to-air missile(AAM)in order to get more data onto analysis and ensure the safety of test range.Considering the limitations of AMM,the paper proposed a parachute-free recovery method,which could control the AMM stably restored by the algorithm.After the recovery demand being analyzed,the corresponding control method was studied.Based on the work above,the recovery algorithm was established by the joint control of track and attitude.In the end,a practical example was given to verify the feasibility of the recovery control method.The tested result showed the algorithm was not only easily practiced but also good execution effect.
作者
何金刚
廖志忠
HE Jin’gang;LIAO Zhizhong(China Air-to-air Missile Academy,Henan Luoyang 471009,China)
出处
《弹箭与制导学报》
北大核心
2020年第4期145-148,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
航空科学基金(20170153002)资助。
关键词
空空导弹
靶场安全
回收控制
控制方法
air-to-air missile
safety of test range
recovery control
control method
