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公开(公告)号：US20230322417A1
公开(公告)日：2023-10-12
申请号：US18208641
申请日：2023-06-12
发明人： Daniel Rey , Farhad Aghili , Franco MOROSO
摘要： An attitude control module is described for providing propellant-free attitude control and momentum desaturation to a spacecraft. The attitude control module includes at least one solar sail comprising a reflective surface for reflecting solar photons; and at least one robotic arm coupled to the at least one solar sail, said at least one robotic arm comprising at least 4 degrees of freedom for positioning and orienting the at least one solar sail relative to the spacecraft. A corresponding method for operating the attitude control module to unload excess momentum from a spacecraft is also described.
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