Tactical Missile Technology

The missile guidance law of the pursuit process was introduced,and a series composite guidance was put forward,such as the whole guidance into the front guidance,proportional guidance law of middle guidance and terminal guidance. The essence was the variable coefficient combination proportional guidance law. Besides,the target aiming algorithm design priciple in the front guidance was introduced.And the proportional guidance law in the middle and terminal guidance was studied. Through the VS2010 and MATLAB,the simulation of three-dimensional missile trajectory was realized. Finally,the visual simulation environment was tested. The results show that the whole design process is effective and feasible,and is consistent with the theoretical analysis consequences.