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绳索联动机构 (CCL)是航天器上最常用的附件同步展开控制机构。本文将其等效为一个被动控制器 ,推导了机构的数学模型 ,分析了其参数对太阳电池阵同步展开的影响 ,并对一大型单翼太阳电池阵的展开过程进行了仿真 ,其结果和实验基本相符。同时得出了一些对工程设计有参考意义的结论
The Rope Linkage (CCL) is the most commonly used attachment deployment control for spacecraft. In this paper, it is equivalent to a passive controller, the mathematical model of the mechanism is deduced, the influence of its parameters on the solar cell array deployment is analyzed, and the unfolding process of a large single-wing solar array is simulated. Experiment basically match. At the same time, some conclusions about the engineering design are given