发明公开
EP1059231A2 Solar array control for a satellite with an electric propulsion system 审中-公开
太阳能电池吊杆用于卫星的控制用的电驱动系统

Solar array control for a satellite with an electric propulsion system
摘要:
In an electric propulsion system (5) used for transferring a satellite to its operational orbit, a solar array adjustment system (13, 14) is controlled to compensate on a continuous basis for the attitude gyrations required by electric thrust vector optimization. The solar array control operates to maintain the solar array in a perpendicular orientation to the sun vector for optimum power generation.
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