- Category:
- Applications
- Tags:
-
- File Size:
- 2kb
- Update:
- 2018-11-03
- Downloads:
- 0 Times
- Uploaded by:
- 北国初雪
Description: After the initial constant is given, the position of the satellite is calculated by iterating the eccentricity anomaly, calculating the angle between ascending node and Greenwich meridian, and the method of calculating satellite velocity is given.
To Search:
File list (Check if you may need any files):
| Filename | Size | Date |
|---|
| 实验1 | 0 | 2017-06-07
|
| 实验1\实验一卫星位置计算例程.m | 5493 | 2017-06-18 |
Download