NANOSATELLITE SUN SENSOR ATTITUDE DETERMINATION USING LOW-COST HARDWARE

被引：0

作者：

Post, Mark A. ^{[1
]}

Li, Junquan ^{[2
]}

Lee, Regina ^{[1
]}

机构：

[1] York Univ, Dept Earth & Space Engn, N York, ON M3J 1P3, Canada

[2] York Univ, Dept Space Sci & Engn, N York, ON M3J 1P3, Canada

来源：

SPACEFLIGHT MECHANICS 2013, PTS I-IV | 2013年 / 148卷

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper outlines the development of two coarse sun sensor methodologies that are compact and efficient enough for a CubeSat-class nanosatellite: direct measurement of the solar angle using a photodiode array sensor, and estimation of the solar angle using current measurements from an array of solar cells. An overview of the technology and hardware designs used is provided in the context of a university nanosatellite development program. Testing results from the sun sensors on a laboratory attitude control system are used to validate and compare the performance of the two methodologies for nanosatellite attitude control.

引用

页码：3773 / 3787

页数：15

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