The present invention relates, in general, to attitude control and, in particular, to control of the attitude of a space platform, conveniently of a satellite and/or a spacecraft. In detail, the present invention concerns an improved logic for controlling a Control Moment Gyroscope assembly (4,6,120) of an attitude control system (100).
ATTITUDE CONTROL FOR AGILE SATELLITE APPLICATIONS
LAGESTEUERUNG FÜR AGILE SATELLITENANWENDUNGEN
CONTRÔLE D'ATTITUDE DESTINÉ À DES APPLICATIONS SATELLITES AGILES
29.08.2018
Patent
Elektronische Ressource
Englisch