The Optimum Intermediate Guidance Law of Missile Considering the Characteristic of Solid Ducted Rocket

It is ideal project to use solid ducted rocket for long distance air to air missile.It is important to consider the characteristic of ducted rocket while researching the guidance law of long distance air to air missile.This paper first presents the means of using dynamic layout to research the guide law which applies to long distance air to air missile using choked ducted rocket.The engineering example confirms the correctness of this means.