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Satellite solar array and method of biasing to reduce seasonal output power fluctuations

机译:卫星太阳能电池阵列及其偏置方法以减少季节性输出功率波动

摘要

Existing satellite solar arrays are deployed perpendicular to the satellite so that they rotate to track the daily movement of the sun to increase the solar array's' output power. In the present invention, the solar arrays (22) are biased by a fixed amount (34) away from the orbit perpendicular axis (32) to maximize their minimum output power over the seasons. As the satellite (20) orbits about the earth, the solar array (22) rotates about the orbit perpendicular axis (32) along a conical path so that the array (22) faces towards the sun and maintains its biased attitude with respect to the sun. The biased attitude is preferably selected to equalize the solar array's summer and winter solstice output power minimums, thereby maximizing the worst case output power for a single axis of rotation solar array (22). The solar array (22) is preferably biased by either forming a shim (54) between the solar array drive mechanism (58) and the solar array (22) with the desired bias (34) or by using the Adjustable Solar Wing Actuator (ASWA) available on certain satellites.
机译:现有的卫星太阳能电池阵列垂直于卫星部署,因此它们旋转以跟踪太阳的每日运动,以增加太阳能电池阵列的输出功率。在本发明中,太阳能阵列(22)被偏置离开轨道垂直轴(32)的固定量(34),以在整个季节中最大化它们的最小输出功率。随着卫星(20)绕地球公转,太阳能电池阵列(22)沿着圆锥形路径绕轨道垂直轴(32)旋转,从而使太阳能光伏阵列(22)面向太阳,并保持其相对于太阳的偏置姿态。太阳。优选地,选择偏置姿态以使太阳能电池组的夏至冬至输出功率最小值相等,从而使单轴旋转太阳能电池组(22)的最坏情况下的输出功率最大化。优选通过在太阳能电池阵列驱动机构(58)和太阳能电池阵列(22)之间以所需的偏压(34)形成垫片(54)或通过使用可调式太阳能机翼致动器(ASWA)来偏压太阳能电池阵列(22) )在某些卫星上可用。

著录项

  • 公开/公告号EP0822138A3

    专利类型

  • 公开/公告日1998-04-29

    原文格式PDF

  • 申请/专利权人 HE HOLDINGS INC. DBA HUGHES ELECTRONICS;

    申请/专利号EP19970112259

  • 发明设计人 SULLIVAN JOHN M.;

    申请日1997-07-17

  • 分类号B64G1/44;

  • 国家 EP

  • 入库时间 2022-08-22 02:49:46

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