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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
/
2012
/
Article
/
Fig 4
/
Research Article
On Bounded Satellite Motion under Constant Radial Propulsive Acceleration
Figure 4
Periodic orbit after
𝜃
=
3
×
2
𝜋
. The red dot in the axis of abscissas is the initial point
𝑟
=
0
.
5
,
𝑅
>
0
.