DocumentCode
3069020
Title
SEDSAT solar array output power analysis
Author
Wang, Yongqian ; Maier, Mark
Author_Institution
Beijing Inst. of Spacecraft Syst. Eng., China
fYear
1998
fDate
8-10 Mar 1998
Firstpage
345
Lastpage
349
Abstract
This paper analyzes SEDSAT´s solar array´s illumination and power conditions. It uses the method of coordinate frame transformation to compute the sun angles on the solar arrays. It defines the solar array´s normal direction in the geocentric orbital coordinate So, and then gets the new normal direction of solar array at the viewer frame (from the sun). The method can be applied on any kind of orbit. It is a numerical calculation method and easily calculated on a computer. This paper also uses a solar array model to calculate SEDSAT´s I-V and power curves. By combining the illumination with solar array´s model, SEDSAT solar panel´s output power profiles are worked out. These results are very useful for evaluating SEDSAT´s power management strategies
Keywords
artificial satellites; solar cell arrays; space vehicle power plants; I-V curves; SEDSAT solar array output power analysis; coordinate frame transformation; geocentric orbital coordinate; numerical calculation method; output power profiles; power curves; power management; solar array illumination; solar array power conditions; sun angles; Aerospace engineering; Earth; Equations; Power engineering and energy; Power engineering computing; Power generation; Satellites; Space vehicles; Sun; Systems engineering and theory;
fLanguage
English
Publisher
ieee
Conference_Titel
System Theory, 1998. Proceedings of the Thirtieth Southeastern Symposium on
Conference_Location
Morgantown, WV
ISSN
0094-2898
Print_ISBN
0-7803-4547-9
Type
conf
DOI
10.1109/SSST.1998.660090
Filename
660090
Link To Document