Recently the research of Satellite Formation Flying (SFF) has increased significantly.
目前关于卫星编队飞行的研究有显著的增加。
Examples of this type of control include formation flying, instrument flight, and landing.
这类操纵的例子包括编队飞行，仪表飞行和着陆。
Based on the nonlinear model, the problem of control for satellite formation flying is investigated.
基于非线性模型，研究了卫星编队飞行的控制问题。
Formation control is one of the important research fields in formation flying around Lagrange point.
拉格朗日点附近编队研究中很重要的一个领域为编队控制。
Readers will fly alongside the Vulcan for 20 minutes before the Blades break away for aerobatics and formation flying.
刀锋特技飞行队表演特技飞行和编队飞行后刀锋特技飞行队飞行员将陪同读者与火神飞行20分钟。
A precision analytical equation to relative motion of formation flying satellites for J2 perturbation is presented.
给出了一种描述J2摄动情况下编队飞行卫星相对运动的精确解析模型。
Multi spacecraft formation flying to form a single virtual spacecraft platform is currently an active research area.
卫星编队飞行组成虚拟平台，这是当前一个完全崭新和开拓性的研究课题。
This measurement method can be used not only for formation flying but also for rendezvous and docking of spacecrafts.
该测量方法可直接用于航天器编队飞行及空间站交会对接过程中的相对姿态测量。
The technology of Formation Flying is a term of crucial technology for the activity of space development in the future.
编队飞行技术是人类进一步开发与利用卫星技术，进行长期深入研究的一项关键技术。
In this paper, the enabling technique of maintenance and reconfiguration control of spacecraft formation flying is studied.
研究小偏心参考轨道航天器编队飞行构形保持与重构控制的工程实现技术。
So both methods of orbit design are suitable for designing orbit of concomitant satellite formation flying around the space station.
用动力学和运动学两种方法研究空间站伴随卫星编队飞行的轨道设计。
The satellite-to-satellite range and time difference measurement were necessary to distributed spacecraft and formation flying systems.
编队飞行卫星间的距离和时间差测量是实现分布式航天器完成特定任务的重要基础。
The formation flying around Lagrange points will benefit deep space exploration greatly due to the special location of the Lagrange points.
由于拉格朗日点的独特空间位置，它附近的编队研究对深空探测有着很重要的意义。
Finally, the formation flying problems near Earth-Moon triangular Lagrange points and corresponding interferometry technologies are studied.
研究了地月三角拉格朗日点编队及基于编队的干涉任务设计问题。
The paper briefly reviews the new research progress of satellite formation flying dynamics and control, and presents some key points for future research.
简要介绍了卫星编队飞行的动力学与控制研究的最新进展，对今 后研究工作的重点提出了建议。
Based on the two-body assumption, two methods are used to investigate the relative motion of satellite formation flying on circular or near-circular orbits.
首先基于二体假设，采用两种方法系统地研究了圆或近圆轨道上卫星编队飞行的相对运动。
The figure of the relative kinematical track of the formation flying will change which is in an ellipse because of the disturbing force from which the satellites suffer.
共面编队飞行的卫星星座的相对运动轨迹是一个椭圆，但卫星由于受摄动力的影响，其椭圆队形会发生变化。
The method will be widely used in many fields such as formation flying of spacecrafts, rendezvous docking with space station, space surveillance and the target holding up.
该测量方法可直接用于航天器编队飞行及空间站交会对接过程、空间监视、目标拦截等应用领域中航天器间相对状态测量。
This paper introduces the characteristics of formation flying small satellites, puts forward a design method for the determination of position and attitude of small satellites.
介绍了编队飞行小卫星特点，提出了小卫星空间状态测量方案。
Considering the differences of attitude change between the member spacecrafts, a hybrid control strategy was designed for spacecraft formation flying using hybrid control techniques.
考虑成员航天器间姿态变化的差异，采用混合控制技术，设计航天器编队飞行混合控制策略。
For enhancing the ability of survivability and auto-control, the requirement of autonomous navigation is brought forward to the formation flying spacecraft and satellite constellation.
为了提高自主生存与自主管理能力，对各类星座及编队飞行的航天器提出了自主导航与定位要求。
In practical applications, some measurement equipment (such as laser) of satellite formation flying can not be used for mission requirements, which led to the decline in observability.
在实际工程应用中，编队卫星由于任务的要求使得部分测量设备(例如，激光设备)不可用，这就造成系统的观测性下降。
For satellite formation flying orbit adjustment situation, which only used radio measurement, a strong tracking unscented Kalman filter (UKF) algorithm was introduced to the simulation.
并针对编队卫星进行轨道机动时仅采用无线电进行测量的工况，采用强跟踪离散卡尔曼滤波(ukf)算法进行仿真计算。
Two clusters of formation flying satellites with a relative angle on geosynchronous earth orbit were used to construct a space-based continuous navigation system for deep space exploration.
介绍了目前各国应用的多种地基和天基空间目标探测与识别系统，并对各系统的性能进行了详细的分析和总结。
To enhance the cooperativity of attitude control for spacecraft formation flying, the synchronization control theory of networks was applied toattitude control of spacecraft formation flying.
文章将网络同步控制理论应用于航天器编队飞行姿态控制，以提高航天器编队飞行姿态控制的协同性。
The attitude coordination control problem for formation flying satellites associated with time-varying reference attitude tracking subject to control input saturation is investigated in this paper.
本文研究了跟踪时变参考姿态情况下的控制输入饱和的编队飞行卫星姿态协同控制问题。
It was showed that PPT was a kind of advanced propeller with small thrust, which was suitable to orbit transfer, attitude control, station keeping and formation flying for small and micro satellite.
分析认为PPT是一种先进的小推力动力装置，特别适合于微小卫星的轨道转移、姿态控制、位置保持以及星座编队飞行。
It was showed that PPT was a kind of advanced propeller with small thrust, which was suitable to orbit transfer, attitude control, station keeping and formation flying for small and micro satellite.
分析认为PPT是一种先进的小推力动力装置，特别适合于微小卫星的轨道转移、姿态控制、位置保持以及星座编队飞行。
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