陀螺光学耦合导引头在机动弹头中的应用技术研究  

Research on the Application of Gyro Optical Coupling Seeker in Maneuver Warhead

作　　者：王伟[1] 王仕成[1] 郭英然[1] 

机构地区：[1]第二炮兵工程学院自动控制系,西安710025

出　　处：《弹箭与制导学报》2005年第S2期312-314,318,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：给出了激光末制导机动弹头系统原理。对陀螺光学耦合导引头进行了全面地分析,建立了导引头数学模型,包括定位原理模型和导引控制模型。对陀螺光学耦合导引头在末制导机动弹头中的应用尤其是对比例导引律的实现进行了论述,为下一阶段末制导机动弹头的仿真研究提供了有效依据。System elements of laser terminal-guided maneuver warhead is given.Gyro optical coupling seeker system is analyzed completely.Its mathematical models are established,including orientating model and guidance system model. The application of gyro optical coupling seeker in maneuver warhead and the realization of proportional guidance are also discussed especially.The pilot study of application of gyro optical coupling seeker in maneuver warhead facilitates fur- ther simulation research.

关 键 词：陀螺光学耦合 机动弹头 比例导引 末制导 

分 类 号：TJ765.331[兵器科学与技术—武器系统与运用工程]