The satellite configuration is the space structure of satellite.
卫星的构形，就是卫星的空间结构。
Analysis of load on the satellite configuration and functionality.
分析了星上载荷的配置和功能。
The positioning accuracy and availability of navigation system are affected directly by the quality of satellite configuration.
在导航系统中，基准站配置的优劣直接关系到定位的精度及系统的可用性。
Parameter design and analysis for satellite configuration can be implemented with this module, and its result can be referenced by other subject design.
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。
Is there any configuration to allow faster access to satellite?
是否有任何配置，以允许更快的连接到卫星？
The fault simulation of satellite attitude control system is crucial for research and experimental verification on optimizing configuration, fault diagnosis, reconstruction of control system.
进行卫星姿态控制系统故障模拟，对控制系统优化配置、故障诊断、系统重构技术研究与实验验证具有重要作用。
This results in a highly optimized satellite platform offering up to 24 channels over a single coax cable when configured dynamically, and in excess of 32 channels in a static configuration.
这导致了高度优化卫星平台时动态地配置，并且在过量的32个信道中的静态配置提供多达24个信道通过单个同轴电缆。
At this point, the satellite is in its final configuration and it will reach its final attitude by correcting the azimuth error as well as the elevation error.
在这个时机点，卫星已经进入最后的设定并且会透过修正方位角错误和仰角错误来达到最后的姿态。
Precise maintenance of formation configuration is a key technique for the application of distributed satellite systems.
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。
In this paper the effect of feed array configuration in satellite multiple beam antennas on pattern synthesis has been investigated.
本文着重研究了卫星多波束天线馈元阵的形状对赋形的影响。
In the proposed schemes, the redundant configuration of grandmaster clock using Beidou navigation satellite system, GPS (Global Positioning system) and atomic clock is discussed.
在应用方案中，讨论了利用北斗卫星定位系统、全球卫星定位系统(GPS)和原子时钟构建最高级时钟的冗余配置方案。
The configuration initialization of satellite formations is carried out based on orbit maneuver control...
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 precision of hanging dynamic model based on CW equation was analyzed in detail, and a low earth orbit satellite octahedron configuration was simulated for validation.
对基于C-W方程的悬停动力学模型进行了精度分析，最后以低轨道航天器的八面体编队构型为例进行了数学仿真验证。
The precision of hanging dynamic model based on CW equation was analyzed in detail, and a low earth orbit satellite octahedron configuration was simulated for validation.
对基于C-W方程的悬停动力学模型进行了精度分析，最后以低轨道航天器的八面体编队构型为例进行了数学仿真验证。
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