摘要
通过对ＭＩＳＴＲＡＭ系统跟踪航天飞行器定轨原理的细致的数学分析，得到了一种解算轨道的新方法。该方法不需要标称轨道，计算极为简便，而且精度高；同时还给出了误差传递方式。实测数据和大量模拟计算均表明，该方法有很好的效果。
n this paper, by means of a detailed mathematical analysis to determine space vehicle orbit's principle of MISTRAM system, have obtained a new method to determine orbit parameters.The method does not need a nominal orbit and it is of easy calcultion and high accurary.Meanwhile, have obtained the law of error propagation.A host of simulated results and calculation of real measured data show that our method is of good efficiency.
出处
《中国空间科学技术》
CSCD
北大核心
1994年第4期1-6,共6页
Chinese Space Science and Technology
基金
国防科技大学预研基金
关键词
MISTRAM系统
误差
航天器轨道
MISTRAM System,Orbit element,Error,Mathematical analysis.
