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.

A fuzzy terminal guidance law with robustness to measurement noise disturbances is presented.

This thesis mainly works on super-maneuverable flight control of fighter, 3D terminal guidance law of air-to-air missile, multi-fighter cooperative multi-target attack, air-to-ground attack and 3D visual simulation.

An optimal terminal guidance law with both interception and impact angle constraint is derived according to simplified missile movement equation and Lagrange method.

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;