CCD组件的热分析和热试验

CCD组件是CCD相机能否传输高质量图片的关键 ,其对工作环境温度的要求非常严格 ,过高或过低的环境温度都会降低其光电转换的能力 ;同时 ,其自身的温度波动过大更会产生热噪声 ,从而使相机的分辨率降低。文章采用NEVADA和SINDA热分析软件计算分析了用电加热功率补偿来保持CCD片温度水平并减小CCD片温度波动的设计方法的可行性 ,得出了几种不同功率补偿方案对CCD组件温度波动的影响。并通过一个热平衡模拟试验验证了热分析的正确性     

一种用于目标特征提取的改进RELAX算法

传统RELAX算法是基于sinc核函数进行处理的，该算法在正弦信号参数估计上具有良好的鲁棒性和有效性。在远场成像条件下，逆合成孔径雷达（ISAR）目标回波可近似为复正弦模型，因而可以采用RELAX算法进行目标特征提取。当对ISAR实测数据进行处理时，复杂目标中强散射中心的高旁瓣电平和噪声的共同影响，造成特征提取中对散射中心的个数估计不准确，影响了特征提取精度。针对这一问题对RELAX算法进行了改进，提出采用加窗处理技术，对RELAX处理的核函数进行修正。数值仿真和对ISAR实测数据的处理结果表明，改进的RELAX算法改善了旁瓣性能，提高了散射中心提取精度。     

Application of GPS to space vehicles: analysis of space environmentand errors

GPS based systems become extremely competitive for space applications because of their all-weather capabilities and continual information on position, velocity, precise time and even attitude to increase mission effectiveness, reduce mission cost, minimize requirements of on-board devices. In this paper, space application environment and error sources have been systematically analyzed, including geometric location of user with GPS satellites, dynamic state, physical environment and the effects on positioning accuracy. Several special differential GPS technologies to space use are proposed     

空地一体化信息对抗系统构架设想

首先介绍“空天一体化”作战体系概念及信息对抗系统的组成和系统特点,并基于目前信息对抗系统的现状和对未来信息战的推测,对空地一体化信息对抗系统构架做了初步的设想.重点介绍空地一体化信息对抗系统的需求、系统构架、组成、特点及关键技术.     

SketchMapia: Qualitative Representations for the Alignment of Sketch and Metric Maps

More and more private citizens collect and publish environmental data via web-based geographic information systems. These systems face two challenges: The user interface must be intuitive and the processing of geographic information must account for cognitive impact. We propose to use sketch maps as the medium for interaction, because they reflect a person's spatial knowledge. Information from sketch maps is distorted, schematized, incomplete, and generalized and metric maps are not. This article employs qualitative representations for the alignment of sketch and metric maps. We suggest a set of cognitively oriented aspects in sketch maps stably computed by people and evaluate qualitative representations to formalize these aspects. This allows us to align and integrate geographic information from sketch maps.     

Design of a high performance suspension for lunar rover based on evolution

In this paper, we propose a new suspension for lunar rover called obverse and reverse four-linkage suspension (ORF-L suspension for short). Its two components are designed based on the evolutions of bogie and rocker. Firstly, we analyze the character of bogie and research the approach to improve its performance. Based on that research, an evolved mechanism of bogie is proposed, named obverse four-linkage. It has better capacity than bogie. In addition an evolved mechanism of rocker is also proposed, named reverse four-linkage. The bogie, rocker and their evolved mechanisms can compose four available suspensions including the interested ORF-L suspension. Because ORF-L suspension is composed of two evolved mechanisms, it has the highest performance. In order to check that, the performance comparison between ORF-L suspension and rocker-bogie suspension are carried out based on simulation. Finally, a prototype rover with ORF-L suspension is designed and manufactured. It shows excellent performance as expected.     

有人/无人机混合编队有限干预式协同决策

针对Leader-Follower异构型有人/无人机混合编队协同决策系统具有递阶分布式决策结构、决策信息分散以及通信约束等特点,在智能体模糊认知图(ABFCM)和动态模糊认知图(DFCM)的理论基础上,提出了一种有限干预式协同决策机制。通过构建层次化的Follower平台自主决策模型,实现了该平台与外部系统良好的交互能力,体现了自主决策的"动态性"。通过设计Leader平台的3种干预策略,满足了不同层次的决策需求,体现了干预过程的"有限性"。仿真结果表明:有限干预协同决策模型能够适应外部环境的动态变化,充分发挥Follower平台的自主决策能力;而不同层次的有限干预介入既减轻了Leader平台的控制负荷,又保证了决策的有效性和可行性,可为解决其他同类复杂系统的协同决策问题提供理论依据和方法参考。     

空间绳系机器人超近距视觉伺服控制方法

针对空间绳系机器人超近距视觉伺服中相对位姿无法测量的问题,在建立机器人视觉系统非线性量测模型的基础上,提出一种基于直线跟踪的混合视觉伺服控制方法,利用帆板支架边缘线图像特征跟踪相对位姿,利用基座具有较大误差的量测信息保证控制系统的稳定性。仿真试验结果表明：在仅能获得帆板支架边缘线图像信息的情况下,设计的超近距逼近控制方法能够保证空间绳系机器人稳定到达目标卫星的帆板支架处,并满足捕获条件。     

航空电子微距太赫兹互连DRR访问容量分析

为了减轻机载电子系统线缆和连接器的重量,减小其体积并降低维护成本,在航空电子组件的电路板或芯片之间,可以采用太赫兹通信技术实现厘米量级的微距互连。采用开关键控（OOK）调制和非相干解调实现点到点太赫兹互连,给出了数据速率、数据包长度等参数的设计方法,进而构建包含用户节点和簇头节点的半双工多路访问分簇网络架构。在簇内用户节点到簇头节点的介质访问控制协议中采用赤字轮询（DRR）机制,并采用随机网络演算（SNC）方法得到概率保证意义下多路访问的有效服务容量,分析了阻塞干扰对DRR服务曲线的影响。分析和算例表明,DRR访问在保证实时性能界限的条件下兼顾了多路访问的灵活性,满足航空电子微小型化组件之间太赫兹通信和分簇组网的需求。     

临近空间高超声速飞行器RCS特性研究

首次系统地对升力体外形临近空间飞行器雷达散射截面（RCS）特性开展了研究,主要研究内容包括本体及绕流RCS特性研究,亚密湍流尾迹RCS特性研究和层流尾迹的RCS特性研究等。结果显示：等离子体绕流将降低飞行器后向RCS;亚密湍流尾迹对低频段RCS影响明显,对高频段影响不明显。另外,双站雷达对临近空间高超声速飞行器也会有较好的探测效果。