To solve the problem in air-to-air missile control parameter design,an automatic control parameter optimization technique is discussed based on particle swarm optimization(PSO) algorithm.

This method are with a high accuracy and real time application,and can be applied in the calculation of allowable launching area of air to air missile in air borne fire control system.

Research on the Control of Air-to-Air Missile at Large Angle of Off-Axis Shot;

Influence of double jet on air-to-air missile with lateral injection control;

Simulation research and overall design for SINS of air-to-air missile;

Design of a 3-D adaptive fuzzy sliding mode guidance law for air to air missiles;

Century scanning on the air to air missile research and development;

An air to air missile is affected by manifold shock and vibration environment when its captive carriage is flying.

This paper narrated process techniques of copper infiltrated tungsten for airborne missile to fabricate jet vane.

By compareing the features and applicability of these two methods,it is suggested that these two methods should be separately used in different stages during the development of an airborne missile.

Life(period of validity) is a key index for airborne missile system,as well for logistic support deployment and combat readiness.