Spacecraft control using residual dipole

    公开(公告)号:US11124320B2

    公开(公告)日:2021-09-21

    申请号:US16273837

    申请日:2019-02-12

    IPC分类号: B64G1/28 B64G1/24 B64G1/32

    摘要: A method for desaturating reaction wheels of a spacecraft having a magnetic dipole is provided. The method includes orienting the spacecraft relative to an external magnetic field to apply a torque to the spacecraft via the magnetic dipole in a direction opposing momentum stored in the reaction wheels; and using the applied torque to unload at least some of the momentum stored in the reaction wheels. A corresponding spacecraft and non-transitory computer-readable medium are also provided.