远程空空导弹的BTT/STT复合控制算法研究  

Research on Hybrid BTT/STT Control Algorithm for Long-range Air-to-Air Missile

作　　者：吕飞[1] 姜殿民[1] 

机构地区：[1]中国空空导弹研究院,河南洛阳471009

出　　处：《计算机仿真》2013年第12期49-52,148,共5页Computer Simulation

摘　　要：在空空导弹飞行转变优化控制问题的研究中,远程空空导弹为了提高射程,一般采用冲压发动机作为动力装置,为了保证冲压发动机正常工作,要求弹体保持较小的攻角和侧滑角。传统方式是采用倾斜转弯(BTT)的控制方式。针对BTT控制方式存在的不足,提出了一种根据控制指令大小选取权系数,将BTT控制与STT控制按照一定的加权原则来实现的BTT/STT复合控制算法。并且根据导弹飞行的不同阶段,提出了BTT-STT切换逻辑,给出了BTT-STT转换算法。最终通过仿真对比分析,验证了提出的BTT/STT复合控制可以解决单独采用BTT控制和STT控制所面临的问题,能够有效地提高控制系统性能。Ramjet is generally used in long - range air - to - air missile to extend the firing range, in order to ensure the normal work of ramjet, the back- to-turn（BTF） control method is applied to maintain little attack angle and sideslip angle. Based on the analysis of the shortcoming of sole BTr control, a hybrid BTT/STT control algorithm was present, which was achieved by a specific method of weighting BTr and STT. On the other hand, the BTT/STT switch logic and transforming algorithm was given by discriminating different fight phase. The simulation result proves the validity of the hybrid BTT/STT control algorithm, which can effectively solve the limitation of sole BTT or STT control, and improve the performance of control system.

关 键 词：远程空空导弹 冲压发动机 控制系统 倾斜转弯 侧滑转弯复合控制 

分 类 号：TJ765.43[兵器科学与技术—武器系统与运用工程]