Modeling and Analysis of the Guidance Loop for the Missile Velocity Pursuit Guidance Law;

In view of physical meanings of body pursuit guidance law,with considering simplified body dynamics,given a heading error as a small perturbation,a linear time-varying model for guidance loop is established.

At last the digital simulation calculation result indicats that the design of the guidance loop can achieve demand of anti-tank missile final guidance.

Study on disturbance rejection rate of a seeker servo system;

Research on 3D Scene Simulation Drived by Missile seeker;

Antijamming performance evaluation of active/passive radar guided seekers of antiship missiles;

An automatic vibration performance test system based on virtual instrument technology for coordinator of homing head is introduced.

This paper introduces the proportional navigation laws and the design of proportional navigation laws for missile control system,it s focus on the math modeling of homing head,the result of the simulation shows that the proportional navigation laws in design of missile control system is effective.

In this paper, the construction and working principle of the simulated target revolving stage control system, which uses 8031 single chip micro-computer as its key part, are introduced, according to the homing head tracking characteristics testing requirement about a certain missile.

Based on a certain pattern, this paper discusses the design guide line and concrete implementation scheme of a general-purpose PD missile header target simulator.