摘要
提出并建立了在地心坐标系下导弹被动段预警弹道的运动方程,将运动方程建立在同一坐标系下进行解算,这一方法突破了以往在导弹发射系求解导弹弹道在预警弹道仿真中的局限,同时有利于仿真子系统间的数据传输。
The missile's trajectory simulation been established. This method broke through the the launch frame of axes and was propitious to th equations based on the earth's core frame of axes have restriction of the separate trajectory simulations based on e data transmission among the simulation subsystems.
出处
《飞行力学》
CSCD
北大核心
2006年第1期63-65,共3页
Flight Dynamics
关键词
地心坐标系
弹道仿真
导弹预警
the earth's core frame of axes
trajectory simulation
missile warning