Name
Abstract | ||
|---|---|---|
•Dynamic modeling of the satellite system with large-scale membrane antenna is developed.•Nonlinear attitude tracking controller and cable actuators are designed to make actual trajectory and desired trajectory of the membrane antenna satellite tend to be consistent.•The stability of these two controllers is proven based on the Lyapunov function. |
Year | DOI | Venue |
|---|---|---|
2020 | 10.1016/j.jfranklin.2020.08.034 | Journal of the Franklin Institute |
DocType | Volume | Issue |
Journal | 357 | 15 |
ISSN | Citations | PageRank |
0016-0032 | 0 | 0.34 |
References | Authors | |
0 | 3 | |