两种位置反馈方法在垂直发射导弹程控段的应用  

Application of Two Kinds of Position Feedback Control Method for Vertical-launched Missile in Program Control Phase

作　　者：朱苏朋[1] 杨军[1] 

机构地区：[1]西北工业大学航天工程学院,陕西西安710072

出　　处：《弹箭与制导学报》2005年第S1期97-99,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：针对某型垂直发射的反舰导弹初始程控段控制方案进行的深入的研究,详细讨论了采用直接欧拉角和伪姿态角两种不同反馈控制方法的优缺点,建立了完整六自由度仿真模型及控制方程,并进行了仿真计算,证明了采用伪姿态角控制方案是可行的。In this paper.Control scheme for vertically-launched missile in program control phase is discussed in detail.Include Euler angle feedback and pseudo attitude angle feedback used in control system,and advantage of each method is compared.At last,Six degree of freedom Simulation model for vertically-launched missile is builded,and result of two method is given.

关 键 词：欧拉角 伪姿态角 垂直发射 

分 类 号：TJ765.2[兵器科学与技术—武器系统与运用工程]