天线(收音机)
参数统计
有效载荷(计算)
计算机科学
电子工程
天线阵
可重构天线
通信卫星
运动学
功率(物理)
工程类
电气工程
电信
航空航天工程
卫星
偶极子天线
天线效率
物理
统计
经典力学
量子力学
数学
计算机网络
网络数据包
作者
Katherine A. Faist,Gloria J. Wiens
出处
期刊:IEEE Aerospace Conference
日期:2010-03-01
卷期号:: 1-8
被引量:13
标识
DOI:10.1109/aero.2010.5446956
摘要
One of the primary concerns associated with the design of small satellites is achieving power capacities sufficient to support payload and mission operations while simultaneously retaining communications capabilities. Furthermore, small satellites must be able to easily transform from their tightly stowed configurations to their fully operational mode. To address these concerns, this paper presents the theoretical modeling and analysis of a class of foldable mechanisms, based on the Hoberman mechanism's kinematic theory, and their parametric coupling with the system parameters of both an antenna array and a solar array. The resulting models provide viable solar array and antenna array designs to generate power and communications capabilities on small satellites.
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