针对预警机协同制导条件下空空导弹的可制导交接区进行研究。在分析基于预警机的空空导弹协同制导流程的基础上, 建立了预警机、发射载机及导弹的力学模型和运动模型, 并从三者自身角度及相互关联的角度分析了影响协同制导交接区的限制因素;在求解协同制导可交接区域过程中, 采用黄金分割法对已建模型进行仿真, 并在仿真中设置了预警机和导弹的不同参数, 根据仿真结果分析参数对制导交接区的影响。结果表明: 在某一确定态势下, 制导交接区与预警机-发射载机通信距离、制导距离、制导天线波束宽度、导弹接收天线波束宽度呈正相关关系; 但当制导天线波束宽度与导弹接收天线波束宽度超过某一定值时, 影响较小。

The allowable guidance handover area of Air-to-Air Missile (AAM) under the cooperative guidance of AWACS is studied.On the basis of analyzing the process of cooperative guidance,the mechanical models and motion models of the AWACS,the launching vehicle and the missile are set up respectively,and the restrictive factors that affect the handover area are analyzed from the aspects of the AWACS,the launching vehicle and the missile and their interrelationship.In the process of calculating the cooperative guidance handover area,the golden section method is used to simulate the model.In the simulation,different parameters of the AWACS and the missile are set respectively.According to the simulation result,the influence of these parameters on the guidance handover area is analyzed.The results show that,under certain situation,the guidance handover area has a positive correlation with the communication distance,the guidance distance,the beam width of the guidance antenna,and the beam width of the missile receiving antenna.However,the influence becomes less when the beam widths of the guidance antenna and the missile receiving antenna exceed a certain value.