太阳帆板绳索联动同步机构的机理和功能分析  

THE RESEARCH ON PRINCIPLE AND FUNCTION OF CLOSED LOOP CONFIGURATION OF SOLAR ARRAYS

作　　者：王天舒[1] 孔宪仁[1] 王本利[1] 马兴瑞[2] 

机构地区：[1]哈尔滨工业大学航天工程与力学系,哈尔滨150001 [2]中国航天科技集团公司,北京100083

出　　处：《宇航学报》2000年第3期29-33,38,共6页Journal of Astronautics

摘　　要：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。Closed loop configuration (CCL) is commonly used as a synchronous deploying control mechanism of appendages.In this paper,the mathematics model is derived based on the consideration that CCL is equivalent to a passive controller.The effect of parameters to the synchronous deployment of solar array is analyzed.In addition,the deployment process is simulated by numerical method,it is shown that the result of simulation agrees that of experiment reasonably well.Meanwhile,some conclusions valvable to engineering are made.

关 键 词：太阳能电池阵 同步展开 绳索联动机构 控制机构 

分 类 号：V442[航空宇航科学与技术—飞行器设计]