1、

However, this algorithm does not apply for circular orbit cone-beam scan with line-focus X-ray source.

但是,这种算法不能满足线X射线源圆轨道锥束扫描的情况。

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2、

I now go into an elliptical orbit because the new velocity is no longer the right velocity for a circular orbit.

我现在要进入一个椭圆形轨道,因为新的速度已经,不是圆形轨道中的速度。

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3、

Post-Newtonian Gravitational Radiation from Binary Stars in Circular Orbit

双星圆轨道的后牛顿引力辐射

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4、

Using the experimental data of circular orbit cone-beam large-field-of-view scan, the reconstruction algorithm creates the right images.

利用这种算法,对圆轨道锥束大视场扫描3D-CT实验数据进行重建,获得了正确的图像。

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5、

Polar crane for nuclear power plant moves on the circular orbit that laying the upper of the reactor plant. It is one of the important hoisting equipments in nuclear power plant.

核电站环行起重机沿着位于反应堆厂房上部的环形轨道行驶,它是核电站中的重要起重设备之一。

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6、

The polar crane for nuclear power plant runs on a circular orbit on the top of the reactor plant, lifts the pressure vessel cover and components for reactor, and the positioning accuracy of polar crane must be strictly controlled.

核电站环行起重机运行于核反应堆厂房上方的环形轨道上,用于吊运反应堆压力容器顶盖和堆内构件,对其吊装定位精度要求极高。

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7、

If the spacecraft into a 185 km high circular orbit required speed of 7.8 km/ s;

如把航天器送入185公里高的圆形轨道运行所需的速度为7.8公里/秒;

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8、

Reconstruction Algorithm for the Circular Orbit Cone-beam Scan 3D-CT with Line-focus Source

线源圆轨道锥束扫描三维CT重建算法

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9、

We have already worked out the conditions for a circular orbit.

我们已经算出了圆轨道的条件。

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10、

Designing on circular orbit constellation of global continuous multiple coverage

持续性全球多重覆盖的圆轨道导航星座的设计

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11、

That also means that the period T must be larger than the period in your circular orbit.

这也意味着,周期T比圆形,轨道的周期大。

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12、

Reasons and Correction of the Artifacts of Single Circular Orbit Cone Beam CT

圆轨迹锥束CT的伪影成因和校正方法综述

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13、

The design method of the orthogonal circular orbit satellite constellation supporting global coverage is studied.

讨论了全球覆盖正交圆轨道星座设计方法。

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14、

Numeral Solution and Analytical Solution of Friction on Object Sliding down on Circular Orbit

物体沿圆弧轨道下滑时摩擦力的数值解与解析解

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15、

Satellite Formation Establishing in Near Circular Orbit

近圆轨道卫星编队捕获技术研究

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16、

Analysis of Orbit Dynamics for Spacecraft Octahedron Formation Configuration in the Circular Orbit

圆轨道航天器八面体编队构型轨道动力学分析

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17、

Possibility of Exact Reconstruction for Cone-beam Projections from A Single Circular Orbit

基于单一圆轨道的锥束投影的精确重建的可能性

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18、

spacecraft into the 1000 km high circular orbit required speed of 8.3 km/ s;

航天器进入1000公里高的圆形轨道运行所需速度为8.3公里/秒;

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19、

Discussion About Closeness of Orbit and Steadiness of Circular Orbit for Motion of Central Forces

有心力运动轨道封闭性与圆轨道稳定性讨论

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20、

An analytical method allowing exact reconstruction from cone-beam projection data which are detected from a single circular orbit is discussed.

本文介绍了一种可以对来自于单一圆轨道的锥束投影数据进行精确重建的分析方法。

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