par Castroviejo Fernandez, Miguel Amando ;Kolmanovsky, Ilya;Garone, Emanuele
Référence Part of special issue: 11th IFAC Symposium on Nonlinear Control Systems NOLCOS 2019: Vienna, Austria, 4–6 September 2019
Publication Publié, 2019
Référence Part of special issue: 11th IFAC Symposium on Nonlinear Control Systems NOLCOS 2019: Vienna, Austria, 4–6 September 2019
Publication Publié, 2019
Publication dans des actes
Résumé : | Translational relative motion of a spacecraft in a gravity field can be induced by orientation changes. As orientation changes can be effected by electrically driven momentum exchange devices, for instance, reaction wheels, such maneuvers do not require fuel or thrust and hence can be performed during propulsion system failures or when the onboard fuel is limited. In this paper, a multi-mode controller is developed to effect such maneuvers which switches between control gains and intermediate target trajectories to extend the closed-loop domain of attraction of a conventional LQR controller and to satisfy state and control constraints. |