Analytic Model for Low Earth Orbit Satellite Solar Power

被引:7
|
作者
Grey, John Petrus [1 ]
Mann, Ian R. [2 ]
Fleischauer, Michael D. [2 ,3 ,4 ]
Elliott, Duncan G. [1 ]
机构
[1] Univ Alberta, Dept Elect & Comp Engn, Edmonton, AB T6G 2R3, Canada
[2] Univ Alberta, Dept Phys, Edmonton, AB T6G 2R3, Canada
[3] CNR, Nanotechnol Res Ctr, Edmonton, AB T6G 2M9, Canada
[4] Univ Alberta, Edmonton, AB T6G 2M9, Canada
关键词
Satellites; Photovoltaic cells; Earth; Sun; Planetary orbits; Computational modeling; Aerospace electronics; circular orbits; low Earth orbit satellites; solar incidence; solar power generation; ORIENTATION;
D O I
10.1109/TAES.2020.3009510
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
An analytic model for calculating the instantaneous and average orbital power available to a satellite in a circular low Earth orbit is presented. By accounting for the effects of angle of solar incidence and eclipsing, for both stabilized and tumbling satellites, this model allows for fast, simple, accurate calculations of available power without the use of complex, often expensive, numerical simulation software. In addition, this method provides the value of maximum and minimum solar power available.
引用
收藏
页码:3349 / 3359
页数:11
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