目前关于卫星编队飞行的研究有显著的增加。
Recently the research of Satellite Formation Flying (SFF) has increased significantly.
基于非线性模型，研究了卫星编队飞行的控制问题。
Based on the nonlinear model, the problem of control for satellite formation flying is investigated.
提出了一种用于小卫星编队飞行控制的星载激光通信兼测距机方案。
A solution of onboard laser-communication - and-laser-range-finder for moonlet formate is introduced.
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。
So both methods of orbit design are suitable for designing orbit of concomitant satellite formation flying around the space station.
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。
Multi spacecraft formation flying to form a single virtual spacecraft platform is currently an active research area.
德国雷达卫星将与在2007年发射的名为TerraSAR - X的卫星编队飞行。
The German radar spacecraft will fly in formation with an identical platform called TerraSAR-X launched in 2007.
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。
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.
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。
The paper briefly reviews the new research progress of satellite formation flying dynamics and control, and presents some key points for future research.
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。
A precision analytical equation to relative motion of formation flying satellites for J2 perturbation is presented.
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 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.
卫星编队的自主运行与管理能够节约大量成本，并能充分发挥卫星编队的整体功能，是编队飞行的关键技术之一。
A key technology for satellites flying in formation is autonomous running and governing, which will reduce the cost significantly and make full use of the whole function of the formation.
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。
The technology of Formation Flying is a term of crucial technology for the activity of space development in the future.
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 satellite-to-satellite range and time difference measurement were necessary to distributed spacecraft and formation flying systems.
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。
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.
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.
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。
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.
根据相对轨道要素的变轨机动控制，进行编队飞行卫星群构型的初始化。
The configuration initialization of satellite formations is carried out based on orbit maneuver control...
本文研究了编队飞行卫星群的轨道动力学特性，提出了编队飞行的轨道构形设计的原则和方法。
This paper reveals the dynamical characteristics of relative orbital motion of formation flight and presents the principles and method for the orbit configuration design of formation flight.
其次，针对编队飞行卫星队形保持控制，以对地等张角绕飞编队为背景设计相对轨道模型预测控制算法。
Secondly, a model predictive control method is designed for the satellite formation keeping and formation of invariant angular to the ground as the background.
其次，针对编队飞行卫星队形保持控制，以对地等张角绕飞编队为背景设计相对轨道模型预测控制算法。
Secondly, a model predictive control method is designed for the satellite formation keeping and formation of invariant angular to the ground as the background.
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