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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
/
2011
/
Article
/
Fig 10
/
Research Article
Planetary Satellite Orbiters: Applications for the Moon
Figure 10
𝑒
versus
𝑔
-degree. Model LP165P. Initial conditions:
𝑖
=
9
0
°,
𝑎
=
1
8
6
1
km. Perturbations:
𝐽
2
–
𝐽
5
and
𝐶
2
2
.