Also, according to the local current balance model, the shaded-side spacecraft potentials under the condition of no photoelectrons are calculated.

并按局部电流平衡模型，计算了航天器背阴面的带电电位。

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In this paper, by using the local current balance model, the charging magnitudes of electrically-isolated, shaded surfaces of a spacecraft are calculated for different shapes and materials.

本文采用局部电流平衡模型，在无光照条件下，对不同表面材料、不同几何形体的航天器充电情况进行了计算。

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