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Home > english-chinese > "orbital parameter" in Chinese

Chinese translation for "orbital parameter"

轨道参数

Related Translations:
orbital axis:  眶轴
orbital decay:  轨道衰减
orbital ferry:  轨道渡运飞行器
orbital storage:  轨道储存量
orbital photograph:  轨道像片
hybridized orbital:  混成轨域杂化轨道杂化轨函数
orbital tracking:  轨道跟踪
orbital resonance:  轨道共鸣轨道共振拉普拉斯共振
orbital symmetry:  轨道对称性轨域对称
orbital spaceflight:  轨道航天技术
Example Sentences:
1.According to the preliminary orbital parameter , no such chance will happen throughout the 5 - day mission . therefore , the whole shenzhou vi spacecraft cannot be seen in hong kong
但根据轨道数据计算,直至五天任务结束时仍没有出现这样的机会,故此本港将不能看见整艘神舟六号。
2.According to the preliminary orbital parameter , no such chance will happen throughout the 5 - day mission . therefore , the whole shenzhou vi spacecraft cannot be seen in hong kong
但根据轨道数据计算,直至五天任务结束时仍没有出现这样的机会,故此本港将不能看见整艘神舟六号。
3.Besides , considering the differences of the galactic gravitational potential models , there is different influence for the distribution morphologies of all of the orbital parameters of the selected sample clusters
此外,不同的银河系引力势模型对所选样本的轨道参数的分布形态也有不同程度的影响。
4.The different galactic gravitational potential have not clear influence upon the perigalactic distance , eccentricity and uncertainty of orbital parameters , but which is significant for other parameters , such as the apogalactic distance , semi - major axis , radial period and azimuth period and so on ; ( 5 ) the monte carlo simulation show that : the distribution morphologies of the orbital parameters which are produced by simulation data are separated into three types : gaussian profile , semi - gaussian profile and non - gaussian profile
不同的引力势模型对近银心距、偏心率和参数的不确定度等量影响较小,但是对远银心距、轨道半长轴、径向周期和方位周期等参数影响较为明显。 ( 5 ) montecarlo模拟的结果表明:根据模拟观测数据得到的轨道参数的分布形态大致可分为三类:高斯分布、准高斯分布和非高斯分布;观测数据对轨道参数的影响与样本的选取、轨道参数的类型等有关。
5.Finally the initial observational data are produced by monte carlo method , and the orbital parameters are calculated using the simulation data for the three sample clusters . the relationship between the distribution morphologies of the orbital parameters and the initial observational date as well as the different galactic gravitational potential models are discussed
最后,对3个样本球状星团的观测数据进行montecarlo模拟,并用于计算它们的轨道参数,以及讨论轨道参数的分布形态与模拟观测数据和不同引力势模型之间的关系。
6.In the stage of the sun and the moon in sight , azimuth of the sun , the earth and the moon in the spacecraft body coordinate system is simulated . combining the simulated azimuth with the ephemeris of the sun and the moon , the state equation and observation equation are modeled . the initial orbital parameters calculated by least square method are used in orbit state equation to predict spacecraft state and to realize autonomous navigation
在日月可见阶段,模拟日、地、月敏感器测量信息,即日、地、月在航天器本体坐标系下的方位信息,结合日月星历,建立状态方程及观测方程,通过最小二乘法得到历元时刻的轨道状态初始值,将其代入轨道状态方程进行自主导航。
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