3D Guidance Law Modeling for Homing Missile;

General missile guidance law is intnxluced briefly.

This paper studies a new guidance law for wide quick pursuit.

A self-adaptive region fuzzy logic guidance law based on Genetic Algorithm and Simulated Annealing;

Simulation design of nonlinear pursuit-guidance law based on sliding-mode control;

A kind of non-buffet discrete variable structure guidance law based on mode reference

Based on the fuzzy logic,a new proportional navigation law is given for the navigation of air-to-air missile.

This paper, based on a large amount of studies on proportional navigation laws, address a pursuit-guidance method for a modern fighter,in which the PPN (Pure Proportional Navigation) is used to pursuit an air adversary which may evade in different modes.

Based on the large amount of study on missile navigation-interception laws and robot control, this paper gives an outline of study results of various proportional navigation laws and addresses the definitions, performances and characteristics of the main type of proportional navigation laws.

With this general state equation,applying a direct feed back linearization (DFL) theory,a accelerate compensation law is reduced,and then based on this compensation law and PN navigation method,an synthetic guidance law is proposed.