在一体化防空作战中,为保证中远程地空导弹在预警机协同下能够精确命中目标。文中在协同制导交接班流程的基础上,提出了两种协同制导交接班方法,并通过建立具有末端攻击角约束的全弹道模型,说明了导弹弹道在交接班过程中的实际作用,最后给出了交接班时间参数计算方法。仿真结果表明,交接班能够在弹道模型中顺利完成,交接班参数计算方法具有有效性和适用性。

In the integrated air defense operation, the medium-long range surface-to-air missile should hit the target accurately under the co-operation of the early warning aircraft. Therefore based on the process of collaborative guidance handover, this paper proposes two methods for collaborative guidance handover. By establishing a full ballistic model with terminal attack angle constraints, the role of missile trajectory in the handover process is illustrated. Finally, the calculation methods of the handover time parameters are provided. The simulation results show that the handover can be successfully completed in the ballistic model, and the calculation methods of handover parameters prove to be effective and applicable.