Kustaanheimo-Stiefel ??????? ???? ???????? ???????? ?????? ????? ????????? ?? ????? ??????? ??????? ?????? ?????? ?????
In this paper the analytic solution for equation of the satellite motion is used to find the Dimension elements for the orbit represented by Semi-major axis and eccentricity, this is done by the effect of the second harmonic J ? 2 of short term orbit for three initial conditions it is seen from it t...
| Main Author: | |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
University of Thi-Qar
2019-06-01
|
| Series: | مجلة علوم ذي قار |
| Online Access: | https://jsci.utq.edu.iq/index.php/main/article/view/501 |