DocumentCode :
260934
Title :
Power limitation method of the solar array regulator for LEO satellites
Author :
Heesung Park ; Hanju Cha
Author_Institution :
Korea Aerosp. Res. Inst., Daejeon, South Korea
fYear :
2014
fDate :
15-18 Jan. 2014
Firstpage :
1
Lastpage :
2
Abstract :
In LEO satellite applications, the regulator can be optimized from the point of mass and volume by limiting the power of the solar array. This paper describes the method how to prevent the over-power generation of the solar array and verifies the proposed method by simulation. The proposed method is simple, so it is easy to apply. In comparison with existing operation mode of the SAR, it is added to one more operation mode, which is a constant power mode. The operation point of the solar array is moved to the voltage area in this mode, therefore the power generated from the solar array is limited. This method can be applicable to other MPPT algorithm such as the P&O and incremental conductance method.
Keywords :
aircraft power systems; artificial satellites; solar cell arrays; solar power; LEO satellite applications; MPPT algorithm; P&O method; incremental conductance method; over-power generation prevention; point-of-mass; power limitation method; solar array regulator; Arrays; Batteries; Low earth orbit satellites; Maximum power point trackers; Regulators; Regulator; SAR; Satellite;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronics, Information and Communications (ICEIC), 2014 International Conference on
Conference_Location :
Kota Kinabalu
Type :
conf
DOI :
10.1109/ELINFOCOM.2014.6914391
Filename :
6914391
Link To Document :
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