CAJ | 학술논문

通过对协同制导交接班的类型进行分析，建立了防空武器系统对AAM（ Anti?aircraft Missile）协同制导交接班的坐标转换模型、误差模型及雷达截获概率模型。通过模拟产生随机误差，利用Monte?Carlo方法进行计算，得出不同误差源对协同制导交接班概率影响的定量关系。实验结果证明了所建模型的有效性，误差分析结论可作为协同制导交接班精度控制的依据。
통과대협동제도교접반적류형진행분석，건립료방공무기계통대AAM（ Anti?aircraft Missile）협동제도교접반적좌표전환모형、오차모형급뢰체절획개솔모형。통과모의산생수궤오차，이용Monte?Carlo방법진행계산，득출불동오차원대협동제도교접반개솔영향적정량관계。실험결과증명료소건모형적유효성，오차분석결론가작위협동제도교접반정도공제적의거。
This article provides a detailed analysis of the components of anti?aircraft missile system and engagement flow. It gives some definition and concept of cooperative guidance. The AAWS ( Anti?aircraft Weapon System) for AAM ( Anti?air?craft Missile) cooperative guidance model is established. It contains concept model of system, coordinate transaction model, errors model and radar tracking probability model. Radom errors are simulated. The Monte?Carlo method is used to have the relationship between errors and cooperative guidance ship probability. The reliable of cooperative guidance model is proved by simulation, which established in this paper. The results of error analysis can be used for precision controlling.