Research of Vertical Launching Missile Based on Turning Control Technology

Turning control of vertical launching missile is one of the most complicated problems in flight dynamics system. This thesis focuses on the design of a high performance control system. Analyze the characters, control demands and performances of vertical launching system; build kinematics equations of vertical launching missile based on quaternion and introduce two control projects of missile turning in this study. One is based on the traditional PD control, and introduces control systems respectively of two turning methods in missile ballistic trajectory; the other is project of active disturbance rejection controller (ADRC) which has so much special performances such as rejecting disturbance, resolving coupling easily, retraining noise and having better robust performances