The particle trajectory is calculated with certain amoune of selected control rules by establishing mathematical mod els such as whole missile mass calculation model,aerodynamic estimation model and turbojet engine performance interpolation.

• 通过建立全弹质量计算模型、气动估算模型和涡喷发动机性能插算等数学模型 ；选取一定的控制规律进行了质点弹道计算 .