Name
Title | ||
|---|---|---|
Adaptive coordinated attitude control for spacecraft formation with saturating actuators and unknown inertia. |
Abstract | ||
|---|---|---|
•The uncertainties of spacecraft formation flying system are unknown time-varying.•The proposed coordination control scheme is robust against inertia uncertainties and disturbances under actuators saturation.•Aiming at optimizing the control algorithm, a dynamic adjustment function is introduced to adjust the control gain according to the tracking errors.•The coordinated controller is designed to track the desired time-varying trajectory under a more practical communication topology.•The presented control law can avoid the system’s chattering. |
Year | DOI | Venue |
|---|---|---|
2019 | 10.1016/j.jfranklin.2018.02.021 | Journal of the Franklin Institute |
Field | DocType | Volume |
Control algorithm,Computer simulation,Control theory,Attitude control,Spanning tree,Inertia,Mathematics,Spacecraft,Actuator | Journal | 356 |
Issue | ISSN | Citations |
2 | 0016-0032 | 1 |
PageRank | References | Authors |
0.35 | 14 | 2 |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Zhihao Zhu | 1 | 3 | 5.13 |
| Guoqiang Yu | 2 | 281 | 39.61 |