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Research on Occlusion of Satellite Solar Array based on Collision Detection Method

机译:基于碰撞检测方法的卫星太阳电池阵遮挡研究

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Protrusions on the satellite surface, especially the antennas might occlude the solar array when the satellite deploying in-orbit. This paper presents a line segment intersection method based on collision detection to simulate and calculate the solar array occlusion. First, the rectangular battery cells of solar array are divided to triangle meshes, and the subdivision degree of the meshes can be improved by linear interpolation. Then, a 3D graph scene is built to simulate the satellite deploying in-orbit. The line segments from the sun point to the entire triangle meshes' center are created, and the intersection between the line segment and satellites' other parts are tested during the real-time rendering process of the scene by the line segment intersection method. Then the occlusion rate can be calculated by the quantity of intersections, and the calculation precision can be improved by increasing the interpolations times. Meanwhile, the occluded triangles of the solar array are rendered to generate the shadow effect to improve the sense of reality. Finally, the method is verified by an example, and the result shows that it has a good precision and a good sense of reality.
机译:当卫星在轨部署时,卫星表面的突起物,特别是天线可能会遮挡太阳阵列。本文提出了一种基于碰撞检测的线段相交方法,以模拟和计算太阳能电池阵列的遮挡。首先,将太阳能电池阵列的矩形电池单元划分为三角形网格,并且可以通过线性插值来提高网格的细分程度。然后,构建3D图形场景以模拟在轨部署的卫星。创建了从太阳点到整个三角形网格中心的线段,并通过线段相交方法在场景的实时渲染过程中测试了线段与卫星其他部分之间的相交。然后可以通过相交的数量来计算遮挡率,并且可以通过增加插值次数来提高计算精度。同时,绘制太阳能电池阵列的遮挡三角形以产生阴影效果,以改善真实感。最后,通过实例验证了该方法的正确性和真实感。

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