Journals
Publish with us
Publishing partnerships
About us
Blog
Mathematical Problems in Engineering
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
Mathematical Problems in Engineering
/
2012
/
Article
/
Fig 4
/
Research Article
Semianalytic Integration of High-Altitude Orbits under Lunisolar Effects
Figure 4
Sample long-term propagations for
Ω
=
0
and
𝜔
=
0
full line, 30 dashed, 60 dotted, and
9
0
deg. dash-dotted. Eccentricity variation.