卫星平台
- 网络Satellite platform;satellite bus
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DFH-4平台是我国新研制的大容量、长寿命静止轨道卫星平台。
DFH-4 is a recently developed GEO satellite platform of China .
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依照报告,第一个阶段是2007年之前一个环月球轨道运行任务,使用DFH-3卫星平台。
According to the report , the first stage is a moon orbiting mission by2007 , using the DFH-3 satellite platform .
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研究了大型柔性卫星平台H∞回路成形姿态稳定控制问题。
The problem of H_ ∞ loop-shaping attitude stabilization control for a large flexible satellite is investigated .
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姿态指向稳定度是合成孔径雷达(SAR)卫星平台设计的重要参数。
Attitude stability is a very important parameter for the platform design of Synthetic Aperture Radar ( SAR ) satellite .
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合成孔径雷达(SAR)通常被装载在飞机或卫星平台上来对地面进行成像。
Synthetic Aperture Radar ( SAR ) is carried on a platform like a plane or a satellite to image the ground .
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小卫星平台的多系统GNSS软件接收机研究
Research on Multi-system Software GNSS Receiver of Micro-satellite
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通过双向捕获的理论模型,分析了光通信终端和卫星平台参量对双向捕获的影响,建立了双向扫描捕获MonteCarlo计算机仿真实验模型。
Using a theoretical model of the bidirectional acquisition , the influences of the parameters of the optical terminal and the satellite on the bidirectional acquisition are analyzed . A model of Monte Carlo experiment was made for the bidirectional acquisition .
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本论文针对卫星平台姿态变化对LASIS成像过程的影响,结合LASIS的成像特点,研究相应的图像校正技术,提出了针对LASIS的图像校正算法。
In this thesis , the image correction technology of LASIS based on satellite attitude changes is studied , taking the imaging characteristics into account .
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未来DRSS系统的发展要求有更高的传输速率,而在现有的卫星平台基础上,必须采用更高阶的调制方式。
Future DRSS requires higher transmission rates , and based on the present satellite platform , modulation modes of higher order must be adopted .
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结果表明,对于100Hz卫星平台角振动,当CCD采样频率大于1kHz时,补偿后的瞄准误差与补偿前相比下降了71%。
It shows that using a CCD with the sampling frequency of 1 kHz , tracking errors can be reduced by 71 % after vibration compensation when the frequency of angular vibrations is 100 Hz .
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研究结论为设计正确有效的LASIS图像校正算法提供了参考依据,同时也为卫星平台设计提供了参考。
Research conclusion provides a reference basis for designing an effective LASIS image correction algorithm , at the same time it also provides a reference for satellite platform design .
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国外高分辨率相机与卫星平台连接方式综述
The Summarization of Connection Ways between Foreign High-resolution Camera and Platform
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其次论述重力梯度小型卫星平台可能达到的技术性能指标;
Then some technical performances of gravity gradient satellite platform are presented .
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卫星平台振动对星间激光链路的影响和解决方案
The effect of vibration on intersatellite optical communication and the resolving project
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储箱平铺多燃料卫星平台的主承力构架结构
Main Heavy Truss with More Fuel of Satellite Platform Structure
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大型柔性卫星平台的变结构姿态控制
Variable structure attitude control of a large flexible satellite platform
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通信卫星平台热分析建模方法研究及温度预示
Research of Thermal Modeling Method and Temperature Prediction for Communication Satellite Platform
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某卫星平台多结构工况下的优化设计
Design optimization of satellite platform considering multiple structural cases
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提出了一种在激光星间链路过程中的卫星平台振动补偿方案。
A method of compensating the satellite vibrations in intersatellite laser links was presented .
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姿态控制系统设计是现代卫星平台的一项关键技术。
Attitude control system design is one of the key technologies of modern satellites .
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在现有条件下,该技术有望率先在极轨卫星平台下得到应用。
This technology can been applied in the polar-stationary satellite platform under the current conditions .
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应用于小卫星平台的中分辨率成像光谱仪
Moderate Resolution Imaging Spectrometer on Small Satellite
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四杆并联机构的卫星平台水平度监控系统研究四边联杆式转向机构
Study on adjustment and control system for satellite platform horizontality Based on 4 DOF parallel structure
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中国空间技术研究院的标准化卫星平台
CAST 's Standardized Satellite Platforms
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首先对测量卫星平台姿态所需要的几种坐标系及其相互之间的转换关系进行了论述。
First of all , this part describes some coordinate systems and the transform relationships between of them .
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本文以考虑边界非线性的蜂窝夹层结构的卫星平台受到起吊冲击载荷作用下的力学特性为工程背景。
The paper 's engineering background was mechanics analysis of satellite base subjected impulsion load considering boundary nonlinearity .
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基于静止气象卫星平台的闪电探测
Lightning Detect on Satellite
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本文的结论将为合理设计卫星平台与空间相机光学系统提供参考。
The results of these analyses can provide references for the reasonable design of the satellite and optical system .
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介绍一种与DJS-1卫星平台及我国卫星测控网适应的卫星测控天线。
A TT C antenna is described suitable for DJS 1 satellite platform and Chinese satellite TT C stations .
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光通信终端与卫星平台的耦合运动是影响卫星光通信系统光信号跟踪性能的重要因素。
The coupled motion of optical communication terminal and satellite platform is the key factor to influence the tracking performance .