Name
Abstract | ||
|---|---|---|
In this tutorial paper we present a novel modeling methodology to derive a nonlinear dynamical model which adequately describes the effect of fuel sloshing on the attitude dynamics of a spacecraft. We model the impulsive thrusters using mixed logic and dynamics leading to a hybrid formulation. We design a hybrid model predictive control scheme for the attitude control of a launcher during its long coasting period, aiming at minimising the actuation count of the thrusters. |
Year | Venue | Keywords |
|---|---|---|
2015 | 2015 EUROPEAN CONTROL CONFERENCE (ECC) | Attitude Control, Sloshing, Hybrid Model Predictive Control, Aerospace |
DocType | Citations | PageRank |
Conference | 0 | 0.34 |
References | Authors | |
11 | 5 | |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Pantelis Sopasakis | 1 | 58 | 11.54 |
| Daniele Bernardini | 2 | 196 | 14.43 |
| Hans Strauch | 3 | 26 | 4.24 |
| samir bennani | 4 | 0 | 0.34 |
| Alberto Bemporad | 5 | 4353 | 568.62 |