1) spatial lamination
空间分片
1.
The spatial lamination method proposed in this paper proves to be an effective way to solve the problem with high speed,good hardware compatibility and adjustable property.
通过使用空间分片的方法可以为浮点精度问题提供了一个解决途径。
2) spatial data fragmentation
空间数据分片
3) ABA,abscisic acid
叶片的空间分布
5) space blade
空间叶片
1.
The method of using three dimensional coordinate instrument to measure the space blade is introduced in this paper.
利用三维坐标仪 ,对一空间叶片进行了定位测量 ,计算出各截面的主要参数 ,根据叶片的受力特点 ,对叶片进行强度校核 ,并对结果进行了理论分
6) orbital debris
空间碎片
1.
SW shield has shown the superior performance compared with the other three structures for protecting spacecraft from meteoroid and orbital debris(M/OD)at an equal areal density and the same imp.
结果表明,在相同面密度条件下,填充式防护结构抗空间碎片的效能最佳,Whipple 防护结构较差,双层铝防护结构介于两者之间,整体式结构最差。
2.
The software of design optimization on orbital debris shielding structure has been initiated in the world on the basis of orbital debris assessment software.
空间碎片防护结构设计优化技术是航天器防护设计的关键技术之一,在空间碎片超高速撞击风险评估软件研制基础上,国际上已开始了空间碎片防护优化软件的研究开发,而且取得了阶段性的研究成果。
3.
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.
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。
补充资料：分片包干
1.划出范围，负责完成任务。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条