摘要
针对不同类型飞航导弹动力装置的工作机理和工作过程,提出了一种兼容发射电路及其控制方法,在原固体火箭发动机飞航导弹发射控制电路基础上,实施兼容性升级扩改设计,通过引入弹上油路状态反馈信号参与导弹发射控制过程逻辑判读、采取继电器串并行复合电气控制,有效满足固体火箭发动机和涡轮喷气发动机两种动力体制飞航导弹的兼容发射。工程实践表明:该飞航导弹兼容发射控制方法简便易行、安全可靠、通用性强、成本低廉。
In accordance with the working mechanism and process of different types of power plants for winged missiles,a compatible launch circuit and its control method are carried out.The compatibility design of upgrade,expansion and reform is implemented based on the original solid rocket engine winged missiles launching control circuit.By introducing the feedback signal of missile oil circuit opening status to participate in the logical interpretation of launch control process,and adopting relays serial-parallel composite electrical control,it effectively meets the compatible launch of solid rocket engines and turbojet engines for winged missiles.The practical application shows that the compatible launch control method for winged missiles is simple and easy to implement,safe and reliable,with strong universality and low cost.
作者
张驰
梁彦
ZHANG Chi;LIANG Yan(No.91851 Troops of PLA,Huludao 125001;No.92941 Troops of PLA,Huludao 125001)
出处
《舰船电子工程》
2025年第7期21-24,共4页
Ship Electronic Engineering
