提出了在比例导引的战术导弹中设计一体化制导控制系统的新思想。依据比例导引的规范要求，以拦截点零跟踪误差为条件，给出了一种最小能量型一体化制导控制器。这种一体化的制导控制器将制导和控制有机地协调一致，克服了传统的比例导引系统的不足，大大提高了导弹的导引精度，仿真结果证明该设计方法是完全可行的。 Proposed in the proportionally guided tactical missile design integrated guidance control system of new ideas. According to the requirements of the proportionally guided specification, a minimum energy integrated guidance controller is given under the condition of zero tracking error of the intercept point. This integrated guidance controller organically harmonizes guidance and control, overcoming the shortcomings of the traditional proportional guidance system and greatly improving the guidance accuracy of the missile. Simulation results show that this design method is completely feasible.