2006•Journal of Projectiles.Rockets.Missiles and GuidanceRequires access

Research on Guidance Law of Air-to-air Missile for High Off-boresight Launch Condition

Fengqi Zhou

Abstract

An guidance law of agile turn of air to air missile in off-borsight launching is discussed.Under thrust vector control,the missile is demanded to maximize the velocity component in parallel director of initial sight in given time,and its final velocity becomes maximum.The digital simulation based on this control law denotes that it possesses very well performance in attacking the targets from the rear hemisphere.

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Key concepts: Air-to-air missile, Missile, Aerospace engineering, Missile guidance, Agile software development, Thrust, Law, Engineering