舰船电子工程2025，Vol.45Issue(7)：21-24,4.DOI:10.3969/j.issn.1672-9730.2025.07.005
飞航导弹兼容发射控制方法的研究与技术实现
Research and Technology Realization of a Compatible Launch Control Method for Winged Missiles
张驰 1梁彦2
作者信息
- 1. 91851部队 葫芦岛 125001
- 2. 92941部队 葫芦岛 125001
- 折叠
摘要
Abstract
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 im-plemented 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-par-allel 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 imple-ment,safe and reliable,with strong universality and low cost.关键词
飞航导弹/兼容发射控制/固体火箭发动机/涡轮喷气发动机Key words
winged missiles/compatible launch control/solid rocket engine/aircraft turbojet engine分类
信息技术与安全科学引用本文复制引用
张驰,梁彦..飞航导弹兼容发射控制方法的研究与技术实现[J].舰船电子工程,2025,45(7):21-24,4.
