The Missile Interface Component Design And Application

This dissertation is on base theory of infrared missile. It's emphases on expatiate design ,develop and produce of the missile interface discreteness.Author using peg-top circumgyrate signal of missile, by phase-locked loops, hase demodulator circuits.Get thereinto two-way signal by way of X and Y benchmark of right angle coordinate,Then,using SCM cortrol,exactitudly drive seeker' s movement and display where it is,by cortrol signal of airplane.The major work of this dissertation is as follows.1. It introduced the function , mostly technique and tactics and control logic of the product. Discuss the part of software and hardware of the product.2. It's expatiate on theory of control and guide of infrared missile , it's brief introduced theory of proportion leading on infrared missile.3. This dissertation emphasis on the part of hardware, the key techniques are some circuits of function and stability for product, for example , phase-locked loops, twisted ring counter circuits, phase demodulator circuits, those elements is the key for control of missile.4. soft ware part is explained for function in the program, for example ,scan module, follow move module, small disarrange module .also, list source code of the program.5. After produced of experimental product. They have did some experiments.conclusion of experiments have been listed. The product has functionality examined, fly experiments, fire control target practice examines, etc, whatsmore, listed some tytical example for some problems.