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The analysis precision of M/OD risk assessment is mostly dependent on the accuracy of space shading algorithm. The M/OD risk assessment plays a very important role in shielding design and in-orbit safety for spacecraft. For the spacecraft shading problem in orbital debris risk assessment, based on Roberts algorithm and Z-buffer algorithm, a shading algorithm is proposed, which is simple in computation, accurate in results and versatile in applications. Spacecraft structures are often very complex, therefore, in the algorithm, a decomposition of the structure and a related shading are made before a combination operation. The shading of simple spacecraft specified by IADC is analyzed. The exposed areas of spacecraft and each finite element in different yawing directions are obtained. The exposed area of the simple spacecraft is different in different directions. The minimum and maximum exposed areas after shading are 38.91% and 55.27% of the exposed area of the simple spacecraft before shading, which shows that the exposed area of spacecraft has great different in different flight attitude. 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科技导报
|研究论文
2009
, 27
(0916) :
36
-39
在轨航天器空间几何遮挡算法
全屏
余庆波1 ,王海福1 ,王辉2
作者信息
1. 北京理工大学 爆炸科学与技术国家重点实验室2. 中国兵器科学院
通讯作者:
王海福
Space Shading Algorithm for On-orbit Spacecraft
Affiliations
出版时间: 2009-08-28
文章导航
航天器空间几何遮挡算法是空间碎片风险评估的关键环节,遮挡算法的正确性对评估精度影响显著。针对空间碎片碰撞风险评估中航天器几何遮挡问题,基于计算机图形学Roberts算法和Z缓冲器算法,建立了一种算法简单、精度高、通用性强的几何遮挡处理方法及算法实现。针对航天器结构比较复杂的特点,提出了先对航天器实现舱段分解,在消除被遮挡面后,再进行合并的遮挡处理原则,并建立了航天器结构空间几何遮挡理论模型及算法流程。采用该算法对IADC规定的简单航天器标准工况进行了遮挡处理分析,得出了遮挡处理后不同方向下航天器的暴露面积。结果表明,不同方向下的航天器暴露面积是不同的,遮挡处理后IADC规定的简单航天器最小暴露面积仅为原来的38.91%,最大也只有原来的55.27%。可见,在不同运行姿态下,航天器暴露面积差别很大,改变航天器飞行路线及运行姿态可有效减少空间碎片的碰撞风险。
Space shading algorithm for spacecraft is the key link of Meteoroid and Orbital Debris(M/OD) risk assessment. The analysis precision of M/OD risk assessment is mostly dependent on the accuracy of space shading algorithm. The M/OD risk assessment plays a very important role in shielding design and in-orbit safety for spacecraft. For the spacecraft shading problem in orbital debris risk assessment, based on Roberts algorithm and Z-buffer algorithm, a shading algorithm is proposed, which is simple in computation, accurate in results and versatile in applications. Spacecraft structures are often very complex, therefore, in the algorithm, a decomposition of the structure and a related shading are made before a combination operation. The shading of simple spacecraft specified by IADC is analyzed. The exposed areas of spacecraft and each finite element in different yawing directions are obtained. The exposed area of the simple spacecraft is different in different directions. The minimum and maximum exposed areas after shading are 38.91% and 55.27% of the exposed area of the simple spacecraft before shading, which shows that the exposed area of spacecraft has great different in different flight attitude. And changes in spacecraft mission operations, flight rules, and flight planning can reduce meteoroid and debris risks.
orbital debris
/
spacecraft
/
shading algorithm
/
exposed area
余庆波;王海福;王辉.
在轨航天器空间几何遮挡算法.
科技导报,
2009
, 27
(0916)
: 36
-39
.
.
Space Shading Algorithm for On-orbit Spacecraft[J].
Science & Technology Review ,
2009
, 27
(0916)
: 36
-39
.
2009年第27卷第0916期
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接收时间:2009-07-16
首发时间:2009-08-28
出版时间:2009-08-28
收稿日期:2009-07-16
修回日期:2009-07-24
https://castjournals.cast.org.cn/joweb/kjdb/CN/1242117086781177982
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2种不同金属材料的力学参数
科 Family 属数 Number of genus 种数 Number of species 占总种数比例 Percentage of total species (%) 属 Genus 种数 Number of species 占总种数比例 Percentage of total species (%) 鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78 小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39 多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39 红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87 小菇属 Mycena 11 5.26 光柄菇属 Pluteus 5 2.39 红菇属 Russula 17 8.13 栓菌属 Trametes 5 2.39
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