micro sun sensor, Japanese space program, small satellite technology, solar sensor, satellite attitude control, CMOS, ground test, thermal vacuum test, vibration test, satellite design
Japan Aerospace Exploration Agency Institute of Aerospace Technology
Japan Aerospace Exploration Agency Institute of Aerospace Technology
Japan Aerospace Exploration Agency Institute of Aerospace Technology
JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
巻
JAXA-SP-06-006
ページ
27 - 32
発行年
2006-11-01
抄録(英)
The Space Technology Demonstration Research Center has conducted the research on a next-generation technology for micro-satellite since 2002. As a part of this research, an experimental manufacture, various test and evaluation of small satellites instruments have been implemented. This paper shows the status of research about the micro sun sensor for attitude control.