Research on Guide and Control Method of Air Launched Ballistic Missile

Abstract

In order to further improve the performance of the air launched ballistic missile, a full range of air launched method had been given. For the full range launch program faced initial roll angle and initial lateral speed problem, researched the initial roll angle control mode processing technology in the virtual body coordinates and correct the lateral initial velocity method used angle of sideslip flight procedures. Given the ballistic flight simulation Using the proposed method and technology, and verified the feasibility of the ballistic missile program of all-round air launched.