| MISTRAM系统定轨的数学方法 |
| |
| 引用本文： | 王正明,周海银.MISTRAM系统定轨的数学方法[J].中国空间科学技术,1994,14(4):1-6. |
| |
| 作者姓名： | 王正明 周海银 |
| |
| 作者单位： | 国防科技大学 |
| |
| 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。
|
| 关 键 词： | MISTRAM系统 轨道要素 误差 数学分析 |
A MATHEMATICAL METHOD FOR MISTRAM SYSTEM TO DETERMINE THE ORBIT |
| |
| Wang Zhengming, Zhou Haiyin.A MATHEMATICAL METHOD FOR MISTRAM SYSTEM TO DETERMINE THE ORBIT[J].Chinese Space Science and Technology,1994,14(4):1-6. |
| |
| Authors: | Wang Zhengming Zhou Haiyin |
| |
| Abstract: | 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. |
| |
| Keywords: | MISTRAM System Orbit element Error Mathematical analysis |
| 本文献已被 CNKI 维普 等数据库收录！ |
| 点击此处可从《中国空间科学技术》浏览原始摘要信息 |
| 点击此处可从《中国空间科学技术》下载免费的PDF全文 |
