Name
Title | ||
|---|---|---|
Model predictive control for spacecraft rendezvous and docking with a rotating/tumbling platform and for debris avoidance |
Abstract | ||
|---|---|---|
A Model Predictive Control (MPC) approach is developed for spacecraft rendezvous and docking to a rotating/tumbling platform and for debris avoidance maneuvers. With this approach, the constraints on thrust, approach velocity and spacecraft positioning within the Line-of-Sight cone from the docking port are systematically treated. The trajectories are simulated and time-to-dock and fuel consumption are evaluated as cost function parameters are varied. Debris avoidance maneuvers are considered, with the debris in the spacecraft rendezvous path. |
Year | DOI | Venue |
|---|---|---|
2011 | 10.1109/ACC.2011.5991151 | American Control Conference |
Keywords | DocType | ISSN |
fuel economy,position control,predictive control,space vehicles,cost function parameters,debris avoidance maneuvers,docking port,fuel consumption,line-of-sight cone,model predictive control,spacecraft positioning,spacecraft rendezvous,tumbling platform,cost function,predictive models,trajectory,center of mass,prediction model | Conference | 0743-1619 |
ISBN | Citations | PageRank |
978-1-4577-0080-4 | 1 | 0.63 |
References | Authors | |
0 | 3 | |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Hyeongjun Park | 1 | 5 | 4.04 |
| S. Cairano | 2 | 249 | 26.23 |
| Kolmanovsky, I. | 3 | 1 | 0.63 |