The hypo-optimal theory was applied on the design of linear quadratic regulator for fast and automatic orbit rendezvous in this paper.
将准最优控制理论用于轨道自主快速交会时线性二次型调节器的设计。
The theoretic analysis and simulation result showed that this control law had high orbit rendezvous precision with little calculation, which could realize fast and automatic orbit rendezvous.
理论分析和仿真结果表明，该控制律的交会精度较高、计算量小，可实现轨道交会控制的自主性和快速性。
The program would be responsible for flight tests of new technologies such as autonomous rendezvous and docking, in-orbit refueling, and inflatable habitat modules.
这个计划将负责进行一些诸如飞行器自动会合和外层空间对接，以及轨道内加油和充气式居留舱等新技术的试验。
One will carry the crew into space, while the other will lift their equipment and supplies to a rendezvous point in orbit.
其中一个搭载机组成员进入太空，另一个将携带他们的仪器和给养至轨道中的交汇点。
The ability to rendezvous in orbit could be used to help clear out space junk or inspect or fix satellites.
轨道相会技术可以被用作清理太空垃圾或是卫星修理。
It was designed to be tested in low Earth orbit so scientists could see various techniques for separation, rendezvous, and dock with the command and service module.
它被设计为在低地球轨道进行测试，以便科学家可以看到分离，聚集各种技术，并与指挥和服务舱对接。
Considering constraints of energy, time and line-of-sight angle, a near-range autonomous rendezvous glidescope orbit design method is studied based on the differential equation method.
考虑能量、时间、视线等约束条件，基于微分方程法研究了近程自主交会滑移轨道设计方法。
The rendezvous and docking (RVD) between two spacecrafts in space involves both orbit control and attitude control with up to 12 degrees of freedom.
空间交会对接涉及到两个航天器同时要进行多达12个自由度的轨道和姿态控制问题。
Near-field autonomous rendezvous orbit design problem is discussed by adopting CW equation in the paper.
采用线性化CW方程研究了空间飞行器近程自主交会轨道设计问题。
The proposed model, control strategy and analysis methods are applicable to the target′s rendezvous orbit design and control implementation.
所提出的计算模型、控制策略和分析方法适用于目标飞行器交会对接轨道设计和控制实施。
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。
According to the target spacecraft's orbit height and the chaser spacecraft's orbit height, the design method of the target's initial phase for the rendezvous orbit was presented.
根据目标飞行器轨道高度和追踪飞行器入轨轨道高度，给出了目标飞行器交会对接轨道初始相位的设计方法。
A stable time-fuel optimal spiral orbit for the rendezvous of an inspector satellite is put forward.
本文设计了一条稳定的燃料-时间优化回收轨道。
An approach for spacecraft autonomous rendezvous in an elliptical orbit without orbit information is developed.
提出了一种在缺少绝对轨道信息时的航天器椭圆轨道自主交会方法。
An approach for spacecraft autonomous rendezvous in an elliptical orbit without orbit information is developed.
提出了一种在缺少绝对轨道信息时的航天器椭圆轨道自主交会方法。
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