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Efficient stationkeeping design for mixed fuel systems

机译:混合燃料系统的高效站场设计

摘要

Apparatus and methods for stationkeeping in a satellite. The satellite includes a north electric thruster and a south electric installed on a zenith side. An orbit controller selects a duration of a burn of the north electric thruster proximate to an ascending node that differs from a duration of a burn of the south electric thruster proximate to a descending node. The orbit controller is configured to select an offset of the burn of the north electric thruster in relation to the ascending node that differs from an offset of the burn of the south electric thruster in relation to the descending node.
机译:用于在卫星中保持位置的设备和方法。该卫星包括安装在天顶一侧的北电推进器和南电。轨道控制器选择靠近上升节点的北电动推进器的燃烧持续时间不同于选择靠近下降节点的南电动推进器的燃烧持续时间。轨道控制器被配置为选择北电动推进器相对于上升节点的燃烧的偏移,该偏移不同于南电动推进器相对于下降节点的燃烧的偏移。

著录项

  • 公开/公告号US9764859B2

    专利类型

  • 公开/公告日2017-09-19

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201514753583

  • 发明设计人 YIU-HUNG MONTE HO;JEFFREY SCOTT NOEL;

    申请日2015-06-29

  • 分类号B64G1/26;B64G1/24;B64G1/40;

  • 国家 US

  • 入库时间 2022-08-21 13:47:32

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