摘要
建立了某型空-地反辐射导弹运动的数学模型,并采用四元数算法描述导弹的姿态运动.给出了雷达定位方法及导弹飞行各阶段的控制信号.最后进行了弹道仿真计算.
Mathematical model of an antiradiation missile—flight is set up.The attitude motion of missile is described by using the quaternions,and radar position is estimated by us- ing the Kalman filter.The control signals in various flight phases of missile arc given.At last, overall trajectory digital simulation is carried out.
出处
《战术导弹技术》
1993年第4期19-23,共5页
Tactical Missile Technology
关键词
反辐射导弹
复合制导
卡尔曼滤波
Antiradiation missile
Modelling
Quaternions
Composite guidance
Kalman filter
