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基于地心坐标系的预警弹道仿真研究
引用本文:雷刚,鲜勇,王明海. 基于地心坐标系的预警弹道仿真研究[J]. 飞行力学, 2006, 24(1): 63-65
作者姓名:雷刚  鲜勇  王明海
作者单位:第二炮兵工程学院603教研室,陕西,西安,710025
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。

关 键 词:地心坐标系  弹道仿真  导弹预警
文章编号:1002-0853(2006)01-0063-03
收稿时间:2004-08-24
修稿时间:2005-08-15

Research of the Trajectory Simulation Equations Based on the Earth''''s Core Frame of Axes
LEI Gang,XIAN Yong,WANG Ming-hai. Research of the Trajectory Simulation Equations Based on the Earth''''s Core Frame of Axes[J]. Flight Dynamics, 2006, 24(1): 63-65
Authors:LEI Gang  XIAN Yong  WANG Ming-hai
Abstract:The missile's trajectory simulation equations based on the earth's core frame of axes have been established.This method broke through the restriction of the separate trajectory simulations based on the launch frame of axes and was propitious to the data transmission among the simulation subsystems.
Keywords:the earth's core frame of axes  trajectory simulation  missile warning
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