Investigation of the Guidance Law for an Image Homing Guidance System

• 作 者: 上官垠黎
• 机 构: North China Institute of System Engineering, Beijing 100089, China
• 出 处: Journal of China Ordnance
• 发表日期: 2005年02期
• 关键词: missile guidance kinematics trajectory proportional disturbance gravity guided n

This paper aims at a type of image homing guided missile. The guided trajectory characteristics and the initial condition of the homing guidance are analyzed by calculating the miss distance of the image guided missile. Several modified proportional navigation laws which are easy for engineering implementation are introduced.

The guided aims and the initial condition of the homing guidance are analyzed by calculating the miss distance of the image guided missile. Several modified proportional navigation laws which are easy for engineering implementation are introduced .