Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
8056114 | Acta Astronautica | 2016 | 20 Pages |
Abstract
In this paper, we study the control and orbit determination problems for elliptical rendezvous. Autonomous rendezvous is achieved by the proposed adaptive control based on the measurements of relative position and velocity between the chaser and target spacecraft. Moreover, the target orbital elements can be estimated during the rendezvous process. Finally, the effectiveness of the method is illustrated by simulations.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Lijia Xu, Yong Hu, Tiantian Jiang,