| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1715036 | Acta Astronautica | 2013 | 13 Pages |
Abstract
⺠General periodic condition is derived at arbitrary position in elliptic orbits. ⺠Zero offset condition is derived to make the leader locate at the formation center. ⺠State transition matrix and energy matching condition approaches are used. ⺠The periodic relative motion is expressed in arbitrary elliptic orbits. ⺠Numerical simulation results show the bounded relative motion in elliptic orbits.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Jonghee Bae, Youdan Kim,