A terminal guidance law based on the terminal sliding mode technology is proposed for the precise interception of exo-atmospheric kinetic interceptor.

A simulation model was developed for endgame homing simulation of kinetic interceptor against mulit-targets.

After constructing the model of motion of the target and the kinetic kill vehicle(KKV),constraints of interception were analyzed and the computing method of orbit transfer was also derived.

In this paper, the kinetic-kill vehicle (KKV), which intercepts tactical ballistic missile (TBM) in the high altitude, is researched.

Optimizing Parameters for KKV Control System Based on Ant Colony and Simulated Annealing Algorithm

Kinetic kill vehicle (KKV) is the primary weapon of the antimissile and antisatellite defence system, the rapidity and the stationary of attitude control system are the key whether KKV can intercept the target or not.

At present,kinetic kill vehicle(KKV)is one of the most successful technology in the anti-ballistic missile weapon system.

Using kinetic kill vehicle to intercept tactical ballistic missile (TBM) during terminal phase, the advantage of Divert and Attitude Control System (DACS) whose response time is very short is taken to improve accuracy and destroy the target by hit-to-kill technology.

This paper studies that the extra atmospheric kinetic kill vehicle intercepts the tactical missile s warhead.

The kinetic kill vehicle operating in higher atmosphere was taken as physical background.