Ultra-high-speed Missile Guidance Technology Research

The research of the control and guide technology for super-speed guided missile is a rather applicable project. This dissertation studies the dynamics of missile in detail, selects rational control and guide technology project, design the system of control and guide and calculate Circular Error Probablity. The main works and contributions of this dissertation are summarized as follows:1. The accurate math model for the system of control and guide is established.2. Studied the general project construction of the automatic pilot for super-speed guided missile.3. The project about the system of control and guide for super-speed guided missile is brought forward.4. Mathematic simulation for the system of control and guide loop in ideal condition, analyze and mathematic simulation for the stabilization loop is progressed on, in order to validate rationality of the design for the system of control and guide.5. The method of precision analysis for the system of control and guide is introduced completely. The result of calculating Circular Error Probablity is offered finally.