卫星载荷1553B总线数据接口的设计与实现CSCD

卫星载荷总线数据流接口的实现对于卫星载荷数据流的传输体制能否正常工作起着关键性的作用,设计合理的数据流管理方案对于卫星载荷之间的正常通信至关重要。MIL-STD-1553B总线数据传输速率高,实时性好,具有合理的差错控制措施和特有的方式命令,适合星上大数据量的传输任务和特定环境的需求。本文使用龙芯配置卫星载荷1553B总线的工作模式,合理设计载荷数据流的传输形式,实现卫星载荷1553B总线的数据流接口。测试结果表明,数据接口可靠性高,实际应用效果好,满足卫星上的通信设计要求。     

基于贝叶斯模型的长码DS-CDMA信号扩频码与信息序列联合估计

 针对长码直接序列扩频码分多址(DS-CDMA)信号的盲解扩,在信号模型分析的基础上,提出了一种基于可逆跳跃的马尔可夫链蒙特卡罗(RJ-MCMC)扩频码和信息序列联合估计算法。该算法分别对建立的联合后验分布模型进行迭代抽样,并有效地在不同维数的子空间中跳转,从而构造一条马尔可夫链,使其平稳分布为待估参数的后验分布,最终拼接得到每个用户的完整扩频序列和信息序列估计。仿真结果表明:该方法在迭代二十几步时达到收敛;并且在功率相同和不同条件下,当信噪比(SNR)大于-9 dB时,估计序列与真实序列的相似度均超过0.95,信息序列的误码率低于0.01;同时算法对不同用户个数和不同调制样式具有较强的适应性,与Fast-ICA算法相比,估计性能平均提高了约3 dB。     

飞机拦阻索动态特性研究

 为了分析飞机拦阻索在拦阻过程中复杂的动态特性,将拦阻索视为空间柔性钢索,液压吸能系统和缓冲系统经过线性拟合,作为传动索的约束条件,通过具有弹性和阻尼特性的梁单元加载在拦阻系统模型中,同时考虑了柔性钢索与刚性支撑体之间的接触碰撞作用,在有限元分析软件LS_DYNA中建立了拦阻系统的碰撞动力学模型,并进行了仿真研究。研究结果表明,飞机尾钩挂索后,在拦阻索与甲板滑轮之间存在连续震荡衰减的应力波,当来自于甲板滑轮的初次反射波到达钩索啮合点时,拦阻力达到极值。     

基于LabWindows/CVI的ARINC429总线数据采集系统设计

首先设计了一套基于LabWindows/CVI的ARINC429总线数据采集系统,该系统采用服务器端和客户端结合的方式,利用线程池的次线程采集数据,并利用异步时钟把数据打包发送给客户端。其次,讨论了两种采集方式对数采系统的影响,并且对ARINC429总线某个Label号的数据失效进行了处理,为以后的ARINC429的数采操作提供了借鉴。     

面向微纳卫星应用的激光数传技术

针对遥感微纳卫星对地高速数传需求,开展面向微纳卫星的激光数传技术研究,突破微纳卫星激光通信终端星地快速捕获建链和协同高精度稳定跟踪、天基终端轻小型化、复合光电组件等关键技术。完成微纳卫星的天基激光终端和地面激光终端研制,并开展星地传输试验验证,实现 1 230 km、10/50/100 Mbps 的星地数据传输,验证了相关技术,为后续我国微纳卫星对地遥感应用提供了理想的星地数传手段。     

Variable slip window technology in transition detection on pitching airfoil

In the pitching motion, the unsteady transition and relaminarization position plays an important role in the dynamic characteristics of the airfoil. In order to facilitate the computer to automatically and accurately calculate the position of the transition and relaminarization, a Variable Slip Window Technology (VSWT) suitable for airfoil dynamic data processing was developed using the S809 airfoil experimental data in this paper and two calculation strategies, i.e., global strategy and single point strategy, were proposed: global strategy and single point strategy. The core of the VSWT is the selection of the window function h and the parameters setting in the h function. The effect of the VSWT was evaluated using the dimensionless pulse strength value (INB), which can be used to evaluate the signal characteristics, of the root mean square (RMS) value of the fluctuating pressure. It is found that: the h function characteristics have a significant influence on the VSWT. The suitable functions are H_n function constructed in this paper and step function. For the left boundary of the magnified area, the step function can obtain the largest INB value, but the robustness is not good. The H₁ function (Gaussian-like function, n = 1) can show higher robustness while ensuring a large INB value. The two computing strategies, which are single point strategy and global strategy, have their own advantages and disadvantages. The former strategy, that is the single point strategy, can achieve a higher INB value, but the RMS magnification at the feature position needs to be known in advance. Although the INB value obtained by the latter strategy, that is the global strategy, is slightly smaller than the calculation results of the former strategy, it is not necessary to know the RMS magnification at the feature position in advance. So the global strategy has better robustness. The experimental data of NACA0012 airfoil was used to further validate the developed VSWT in this paper, and the results show that the VSWT developed in this paper can still double the INB value of the transition/relaminarization position. The VSWT developed in this paper has certain practicability, which is convenient for the computer to automatically determine the transition/relaminarization characteristics.     

惯性基准系统内部接口问题分析

介绍了惯性基准系统的组成及原理．详细分析了惯性基准系统上电后一直工作于Align模式而无法进入Nav模式的故障，分析认为其原因是RS-232C接口的通信距离与负载电容大小有关。因此为了减少负载电容，保证数据的通信正确，只能减少屏蔽双绞线上的分布电容．即限制电缆的长度。     

卫星舱内无线传输技术的应用探索

针对传统有线连接的整星电缆网其灵活性差、通用性差及操作性差等问题,提出了利用无线网络通信技术解决卫星舱内有线连接在整星布局、装配、集成和测试等方面的不利影响,进行了基于卫星舱内使用的无线传输网络设计和探索,包括无线网络拓扑结构、网络频率配置及通信抗干扰等内容。通过基于某型号卫星的数据传输应用场景进行了方案设计和试验测试,验证了卫星舱内无线传输技术的可行性,为解决卫星平台和有效载荷之间的数据交换和平台自身管理提供了一个高可靠、高效率的实现途径。     

Analysis of laser ranges and angular measurements data fusion for space debris orbit determination

In the framework of space debris, the orbit determination process is a fundamental step, both, for researchers and for satellite operators. The accurate knowledge of the orbit of space debris objects is needed to allow space debris characterization studies and to avoid unnecessary collision avoidance maneuvers.The accuracy of the results of an orbit determination process depends on several factors as the number, the accuracy, the kind of processed measurements, their distribution along the orbit, and the object-observer relative geometry. When the observation coverage of the target orbit is not homogeneous, the accuracy of the orbit determination can be improved processing different kind of observables. Recent studies showed that the satellite laser ranging technique can be successfully applied to space debris.In this paper, we will investigate the benefits of using laser ranges and angular measurements for the orbit determination process. We will analyze the influence of the number of used observations, of the covered arc of orbit, of each observable, and of the observation geometry on the estimated parameters. Finally, using data acquired on short observation arcs, we analyze the achievable accuracies for the orbital regimes with the highest space debris density, and to the consequences of the data fusion on catalog maintenance operations. The results shown are obtained using only real data (both angular and laser measurements) provided by sensors of the Swiss Optical Ground Station and Geodynamics Observatory Zimmerwald owned by the Astronomical Institute of the University of Bern (AIUB) and for some studies also using ranges provided from other stations of the International Laser Ranging Service (ILRS).     

星载原子钟数据预处理的方法研究CSCD

星载原子钟的数据预处理是进行原子钟性能分析和钟差预报的前提,本文主要利用相位数据和频率数据的转换和异常数据的分析处理方法对原子钟数据进行了预处理,有效的保证了数据的可靠性。