A structure and control system for changing the attitude of an object, such as a spacecraft, is provided. An example attitude control system includes a panel coupled to the object. The panel includes a first panel section coupled to the object by way of a first joint, a second panel section coupled to the first panel by way of a second joint, and a third panel section coupled to the second panel by way of a third joint.
MULTIFUNCTIONAL STRUCTURES FOR ATTITUDE CONTROL
24.03.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |