Analysis of solar panel orientation in low altitude satellites

Anigstein P.A.; Sanchez Pena R.S.

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Analysis of solar panel orientation in low altitude satellites

机译：低空卫星的太阳能电池板定向分析

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The computation of the optimal orientation of solar panels which are fixed to the body of the satellite, from the point of view of average power, is presented. In practical cases, some of the parameters which determine the optimal orientation vary during the lifetime of the satellite. In these cases we compute a worst case optimum, which maximizes the average power in the worst case situation. Finally, an application of these procedures to an Earth observation satellite is performed

机译：从平均功率的角度，介绍了固定在人造卫星上的太阳能电池板最佳方位的计算。在实际情况下，确定最佳定向的某些参数会在卫星的使用寿命内发生变化。在这些情况下，我们计算最坏情况下的最优值，从而在最坏情况下最大化平均功率。最后，将这些程序应用于地球观测卫星

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《IEEE Transactions on Aerospace and Electronic Systems》 |1998年第2期|p.569-578|共10页
作者
Anigstein P.A.; Sanchez Pena R.S.;
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正文语种 eng
中图分类航空;
关键词
artificial satellites; optimisation; solar absorber-convertors; solar cell arrays; space vehicle power plants; Earth observation satellite; Sun projection; average power; daylight angle; eclipse computation; effectiveness coefficient; fixed panel orientation proble;

机译：人造卫星;优化;太阳能吸收器-转换器;太阳能电池阵列;航天器动力装置;地球观测卫星;太阳投影;平均功率;日光角;日食计算;有效性系数;固定面板方向性问题;

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1. Analysis of solar panel orientation in low altitude satellites [J] . Anigstein P.A., Sanchez Pena R.S. IEEE Transactions on Aerospace and Electronic Systems . 1998,第2期

机译：低空卫星的太阳能电池板定向分析
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Analysis of solar panel orientation in low altitude satellites

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