Sliding Mode Control of Moving-Mass-Center System for Terminal Guidance of Ballistic Missile;

Technology Research on Synthetic Aperture Radar Terminal Guidance;

Research on nonlinear terminal guidance law under high alignment angle condition;

Robust terminal guidance law for maneuvering targets;

Considering the attack process of the television guidance UCAV,taking a terminal guidance law of UCAV as a problem of tracking the target at meeting the impact attitude angle restriction,the law based on autopilot was designed,which eliminates the influences of dynamic factor of autopilot and gravity factor on hitting the target.

Selecting appropriate terminal guidance law is an important factor for the precise guidance of anti-ship missile.

Analysis on Side Jet/Aerodynamics Compound Control of Air-to-Air Missile in Endgame;

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.

The start time of terminal guidance radar is unknowable,which results in the realization of dilution jamming is difficult.

In basic framework of total system,signal stage,isomorphic simulation for centroid chaff countering anti-ship missile terminal guidance radar,models of warship were researched.