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Simulation Approach to Determine Position of the Fixed Installed Deployable Solar Panel

机译：确定固定安装的可展开太阳能电池板位置的仿真方法

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摘要

The popularity, development and promising performance in orbit for small satellite make it's trends of mission to be run by the satellite become more complex. Since the small satellites may brought payload with higher power requirement to run its mission. This payload may not be able supported by the power system, in which is a combination of solar panel with batteries. Small satellite also has size and mass constraints which made it won't be able to bring active motion mechanism for the solar panel. A natural question to be answered is where the best installation position (placement) of the deployable solar panel with respect to the body satellite such that the power system can acquire maximal solar energy. This paper proposes simulation based method to determine placement (position) of the fixed installed deployable solar panel system such that maximal power can be provided. To validate this method, simulations data summary is presented in this paper where concerns in two different orbits of satellites and eleven cases that accommodates. Based in the simulation results, options for the position of the fixed installed deployable solar panel is provided.
机译：小型卫星在轨道上的普及，发展和有希望的性能，使得由卫星运行的任务趋势变得更加复杂。由于小型卫星可能会带来更高功率要求的有效载荷来执行其任务。电力系统可能无法支持此有效负载，该系统是太阳能电池板与电池的组合。小型卫星还具有大小和质量限制，这使其无法为太阳能电池板带来主动运动机制。一个自然要回答的问题是可展开的太阳能电池板相对于卫星的最佳安装位置（位置），以便电力系统可以获取最大的太阳能。本文提出了一种基于仿真的方法来确定固定安装的可部署太阳能电池板系统的放置（位置），以便可以提供最大功率。为了验证该方法，本文提出了仿真数据摘要，其中涉及两个不同的卫星轨道以及可容纳的11种情况。根据仿真结果，提供了固定安装的可展开太阳能电池板位置的选项。

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