公开(公告)号：US20040122568A1

公开(公告)日：2004-06-24

申请号：US10687585

申请日：2003-10-20

Applicant: ALCATEL

Inventor： Eric Montfort ,  Cedric Salenc ,  Xavier Roser ,  Loic Gaudic

IPC: G05D001/00 ,  B64C001/00 ,  G05D003/00 ,  G06F007/00 ,  G06F017/00

CPC classification number: B64G1/244

Abstract: An attitude control system is disclosed for geostationary satellites including elongate members such as solar generators and/or antennas, in particular deployable members. The system includes gyroscopic actuators for supplying the torque necessary for maintaining the attitude of the satellite when subjected to disturbing forces or torques. The gyroscopic actuators preferably maintain a setpoint attitude during orbit correction phases.

Abstract translation: 公开了一种用于对地静止卫星的姿态控制系统，包括诸如太阳能发电机和/或天线的细长构件，特别是可部署的构件。 该系统包括用于在受到扰动力或扭矩时提供用于维持卫星的姿态所必需的扭矩的陀螺仪致动器。 陀螺式致动器优选地在轨道校正阶段保持设定点姿态。