Research on missile formation control system

The control system of missile formation flight is described. In this paper, the missile formation flight controller and BTT intelligence missile outer-loop controller are interested. A combination of proportion and differential control of the position error is used in the designing of the missile formation flight controller to generate the control command for the single missile. The missile outer-loop controller is designed based on the total energy. Simulation demonstrate that the missile formation controller are capable of controlling the missile formation and the BTT missile controller can track the command generated by the missile formation controller exactly.