Name
Abstract | ||
|---|---|---|
This paper investigates the robust H∞ control problem of spacecraft rendezvous on elliptical orbit. Based on Lyapunov theory, a sufficient condition for the existence of the robust H∞ controller is given in terms of the periodic Riccati differential equation (RDE). Then, a stabilizable controller design method based on a fast multi-shot algorithm is proposed. With the controller obtained, the spacecraft rendezvous mission can be accomplished. An illustrative example is provided to show the effectiveness of the proposed control design method. |
Year | DOI | Venue |
|---|---|---|
2012 | 10.1016/j.jfranklin.2012.08.005 | Journal of the Franklin Institute |
DocType | Volume | Issue |
Journal | 349 | 8 |
ISSN | Citations | PageRank |
0016-0032 | 2 | 0.45 |
References | Authors | |
2 | 3 | |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Xiangyu Gao | 1 | 3 | 2.17 |
| K. L. Teo | 2 | 1643 | 211.47 |
| Guang-Ren Duan | 3 | 1735 | 177.31 |