space rendezvous

This paper presents the approaches and practical theoretical models on synthetic orbit maneuver during long distance guidance stage of space rendezvous.

文章研究了空间交会远程导引阶段综合变轨问题的变轨策略方法和实用理论模型。

Space rendezvous and docking station is built on the basis of technology.

空间交会对接是建立空间站的基础性技术.

Shenzhou-8 is expected to perform China's first-ever space rendezvous and docking when it joins up with Tiangong-1, or Heavenly Palace-1, a space lab module sent into space in late September.

神州8号有望执行我国首次空间交会对接任务，与九月下旬送入太空的空间实验模块&天宫一号联结。

A manned ShenZhou-11 capsule is set to launch in October, carrying two astronauts, to rendezvous and dock with the TianGong-2 space station precursor facility in low Earth orbit.

载人神舟11船舱将在十月发射，搭载两名宇航员，会合，并在地球低轨道的天宫二号空间站前体设施对接。

Tiangong I had completed six space rendezvous and docking missions with three visiting spacecraft.

天宫一号已经完成了6次空间交会，并和3艘飞船实现了对接。

After that, an elliptic orbit two-impulse guidance method is introduced. Furthermore, this paper also gives a kind of nonlinear guidance method for space rendezvous.

最后，在椭圆参考轨道相对运动模型的基础上，研究了椭圆参考轨道的二脉冲交会制导策略。此外，本文还给出了一种空间交会的非线性制导方法。

That will change early next year when the 2 astronauts rendezvous at the International Space Station.

这种局面明年早些时候就会改变.两兄弟将在国际航空站相见.

MATCH POINT The ideal rendezvous time, launch time and rendezvous point in space were studied.

研究了标称飞行轨道最优交会点选取，交会时间与发射时间计算等问题。

Research on Algorithm of Loopy Lambert Transfer in Space Rendezvous

空间交会中多圈Lambert变轨算法研究

Based on the combination of a tangential impulse maneuver and a constant continuous radial thrust maneuver, a new strategy for space V-bar rendezvous was presented.

提出了一种基于切向脉冲与径向连续常推力组合机动的空间V-bar交会策略。

The problem on orbital rendezvous of spacecraft is a crucial technology for human space exploration. It is one of the most difficult problems in theory and application of spacecraft control.

空间在轨交会是载人航天技术中的关键问题之一，是目前航空控制理论与实践中的难点之一。

An improved adaptive filter is proposed in this paper for measurement noise uncertainty during rendezvous& docking with non-cooperative target in space.

针对空间非合作目标对接过程中特征点识别的非高斯测量噪声与幅值不确定，对传统滤波方法的量测更新部分进行改进。

Homing Mission Design of Space Rendezvous Based on Proportional Guidance

基于比例导引的空间交会寻的段飞行任务设计

Finally, this paper tried to start a new research field that named as Rendezvous Area and Space Control Body, by introducing these concept, visualization for large scale orbital maneuver was able to show directly.

最后，论文尝试性的提出并研究了点对面的机动及追踪器控制体的概念，给出了高度直观的大范围轨道机动可及范围，从面的覆盖的概念上分析得到了最佳机动时限。