A structure for changing the attitude of a spacecraft is provided including an elongated member and a plurality of actuators coupled to the elongated member. The elongated member is coupled to the spacecraft. The elongated member has a length and an angular position relative to an axis. The plurality of actuators are configured to deflect the angular position of the elongated member relative to the axis and to alter the length of the elongated member.
MULTIFUNCTIONAL STRUCTURES FOR ATTITUDE CONTROL
MULTIFUNKTIONSSTRUKTUREN ZUR LAGEREGELUNG
STRUCTURES MULTIFONCTIONNELLES POUR LA COMMANDE D'ATTITUDE
2023-06-21
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |