巡航导弹中制导精度分析与仿真

Precision Analysis and Simulation of Cruise Missile Middle Guidance

对于中远程巡航导弹来说,中制导段的飞行时间长、距离远,是巡航导弹完成任务的关键。本文以假想的巡航导弹设计为背景,对影响巡航导弹中制导精度的各种因素进行分析,最后通过仿真得到了相关的误差模型。这项工作,为巡航导弹中制导的设计提供了参考依据。

Middle guidance is pivotal for long-distance cruise missile to achieve mission because of its long time fly. Base on one cruise missile, this paper analyzes the factors to influence the middle guidance precision of cruise missile, and makes simulation. The study will afford a reference for the design of cruise missile middle guidance.