该插件实现了卫星构形的参数化设计和分析，其分析结果为其它学科的设计提供参考和依据。
Parameter design and analysis for satellite configuration can be implemented with this module, and its result can be referenced by other subject design.
通过对绕飞编队特性的研究，提出了一种适于摄影测量的卫星绕飞编队构形。
According to the study of the performance of the satellite flying-around formation, a formation suit for photogrammetry is proposed.
研究近地轨道卫星编队构形在引力摄动作用下的长期演化机理。
The mechanism of Low earth orbit(LEO) satellite formation secular evolvement under the influence of gravitational perturbations is studied.
编队构形精确保持控制是实现分布式卫星系统的关键技术之一。
Precise maintenance of formation configuration is a key technique for the application of distributed satellite systems.
针对卫星编队轨道构形在J2摄动干扰作用下被破坏的问题，给出了两种构形保持脉冲控制策略。
Two impulsive control strategys for formation keeping were put forward with regard to the problem that satellites formation could be destroyed under J2 perturbation.
卫星的构形，就是卫星的空间结构。
The satellite configuration is the space structure of satellite.
文章介绍了整平船的结构形式、设备配置及先进的卫星定位系统、测量系统。
This paper presents the structure form of leveling barge, equipment disposition and the advanced system of satellite positioning and photogrammetry.
构形设计是卫星一项重要的总体方案设计工作。
Its design is an important part of the system concept design.
星座构形可由卫星相对地球的位置和卫星相对卫星的位置联合描述。
The architecture of a constellation can be described jointly by the position of the satellite relative to the earth and the position of the satellite relative to other satellites in the constellation.
在太阳同步轨道卫星上应用的辐射制冷器都采用两级抛物面w型的结构形式。
The radiant cooler used in the sun synchronous orbit is always designed two stages with a W-shaped parabolic reflector.
周边桁架可展开天线结构形势简明，工作原理清晰，是目前大型卫星天线理想的结构形式。
The flexible cable net deployable antenna have a simple structure and distinct working theory, so it is the ideal structure form of large satellite antenna at present.
首先，简介主SAR卫星与伴随卫星编队所构成干涉测量系统的工作原理，当主SAR卫星施加偏航导引补偿多普勒频移时，为实现波束指向同步，伴随编队需进行构形与姿态的协同控制。
When SAR satellite compensates Doppler Shift with yaw steering, for beam pointing synchronization, formation maintenance and attitude control of concomitant satellite formation should be coordinated.
编队卫星轨道设计与构形保持的主要目的就是以较小的代价满足这两个约束。
The purpose of the formation design and station keeping is satisfying two constraints with the least propellant cost.
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.
并且根据卫星群偏心率与倾角综合的分离思想，讨论了两种策略，使得卫星群的构形可通过每个成员的轨道要素简单表出。
The satellites follow a combined eccentricity and inclination vector separation strategy, so that the group geometry can be expressed simply by the orbital elements of each member.
随着卫星种类、结构形式的不断变化，卫星对包带装置提出了更高的要求。
With the gradual development of the satellitic sort and structure, the improvement of clamp band is needed. So it becomes more and more important to research its dynamic envelope simulation.
随着卫星种类、结构形式的不断变化，卫星对包带装置提出了更高的要求。
With the gradual development of the satellitic sort and structure, the improvement of clamp band is needed. So it becomes more and more important to research its dynamic envelope simulation.
应用推荐