绳索断裂对二维二次太阳翼展开过程影响分析

为识别二维二次太阳翼关键环节和预示其在轨展开故障模式，开展不同位置绳索断裂失效对太阳翼展开的影响程度分析。采用考虑绳索断裂的绳索联动轮力学模型，建立了适应于不同联动轮半径的联动轮受力模型，提出角度触发约束消除方法，解决了太阳翼第2次展开过程连续仿真问题，建立了太阳翼第2次展开动力学方程，分析了不同位置绳索断裂失效对太阳翼各板展开角度、展开构型和其他绳索张力的影响。分析表明，越靠近星体的绳索联动机构失效对太阳翼展开过程的影响越大，其中连接架上绳索联动机构失效可直接导致二维二次太阳翼在轨展开失败。     

双向比对高精度物理时间同步方法

提出一种面向未来卫星在轨应用的闭环物理高精度时间同步方法。比较了所提方法与其他时间同步方法的区别与优势，建立了远程系统时间同步基本模型与误差传递模型，基于双向测距和时间传递技术分析了高精度钟差获取原理，给出了时钟调整环路的时域频域参数依赖关系。完成了高精度时间同步地面试验系统构建，测试了开环非调钟状态下钟差测量精度误差、闭环调钟状态下时间同步准确度误差以及长时运行情况下的时间同步监测结果。测试结果表明，该方法能够实现优于1 ns量级的时间同步，为高精度时间同步技术研究提供了新的途径。     

An innovative study on low surface energy micronano coatings with multilevel structures for laminar flow design

Laminar flow design is one of the most effective ways to reduce the drag of a commercial aircraft by expanding the laminar flow region on the surface of the aircraft. As material science develops, the emergence of new materials such as low surface energy materials has offered new choices for laminar flow design of commercial aircraft. Different types of low surface energy micro-nano coatings are prepared to verify the effects on the boundary layer transition position and the drag of the airfoil through wind tunnel tests. The infrared thermal imaging technology is adopted for measuring the boundary layer transition, while the momentum integral approach is employed to measure the drag coefficient through a wake rake. Infrared thermal imaging results indicate that the coatings are capable of moving backward the boundary layer transition position at both a low velocity of Mach number 0.15 and a high velocity of Mach number 0.785. Results of the momentum integral approach demonstrate that the drag coefficients are reduced obviously within the cruising angle of attack range from 1° and 5° by introducing the low surface energy micro-nano coating technology.     

AADL在航天器控制系统设计中的应用研究

以某型号航天器为例提出了一种使用体系结构分析和设计语言(AADL,architecture analysis & design language)分层次建模的方法,建立控制系统软件及软件与硬件之间的交互模型.采用状态自动机方式描述串口通信协议,以便分析模型.     

Exploiting global information in complex network repair processes

Robustness of complex networks has been studied for decades,with a particular focus on network attack.Research on network repair,on the other hand,has been conducted only very lately,given the even higher complexity and absence of an effective evaluation metric.A recently proposed network repair strategy is self-healing,which aims to repair networks for larger compo nents at a low cost only with local information.In this paper,we discuss the effectiveness and effi ciency of self-healing,which limits network repair to be a multi-objective optimization problem and makes it difficult to measure its optimality.This leads us to a new network repair evaluation metric.Since the time complexity of the computation is very high,we devise a greedy ranking strategy.Evaluations on both real-world and random networks show the effectiveness of our new metric and repair strategy.Our study contributes to optimal network repair algorithms and provides a gold standard for future studies on network repair.     

抗辐射保偏光纤的制备及其特性研究

通过对保偏光纤进行光漂白与低温相结合处理的方式，来提高光纤的抗辐射性能。保偏光纤再经过1.0 kGy的高剂量预辐照处理后，其损耗会明显增大。随后采用980nm的激光对光纤进行光漂白处理,其损耗并没有发生明显变化。但是，处理后的样品在小剂量辐照条件下其光纤传输呈现先减小后增大的趋势。对于通过液氮进行冷处理的预辐照样品，其光纤传输损耗得到明显的降低，同时光纤经过小剂量辐照后的损耗同样也具有先减小后增大的现象。最后，将两种处理方式相结合，一方面可以有效地降低预辐照光纤的传输损耗，另一方面也使得保偏光纤在小剂量辐照的条件下，使其传输损耗具有减小的趋势，大大提高了保偏光纤在小剂量辐照条件下的抗辐照特性。     

精密露点仪标准装置的性能测试及计量软件设计

文章介绍了以373型精密露点仪为主标准器的湿度标准装置的原理及构成,对该装置的重复性和稳定性进行了测试。结果表明温度重复性实验的标准偏差为0.00℃,相对湿度重复性实验的标准偏差为0.07%RH,露点温度重复性实验的标准偏差为0.01℃。温度稳定性实验的标准偏差为0.02℃,相对湿度稳定性实验的标准偏差为0.33%RH,露点温度稳定性实验的标准偏差为0.066℃。基于美国NI公司的Labview软件开发平台,开发了湿度仪器仪表计量软件。软件以模块化思想为基础,可实现数据自动处理,报告自动生成。     

纤维增韧陶瓷基复合材料的比例极限应力与残余热应力关系

从细观力学角度分析并建立了纤维增韧陶瓷基复合材料从制备温度冷却到室温过程中产生的残余热应力与复合材料的比例极限应力的关系模型。该模型表明,减少复合材料的残余热应力或提高复合材料的纤维与基体的模量比,均可提高复合材料的比例极限应力。通过单调拉伸实验测试了先驱体浸渍裂解法(PIP)制备的2D SiC/SiC复合材料的比例极限应力,并采用文中建立的比例极限应力与残余热应力关系模型,计算出复合材料SiC基体的残余热应力为-19.5 MPa。分析表明,该结果是合理的。此外,引用了公开文献报道的5种复合材料体系数据,用于验证文中所建立的比例极限应力与残余热应力关系模型的适应性和可靠性,计算结果与实验结果最大误差为18.6%,表明该模型具有较好的适应性和可靠性,可为纤维增韧陶瓷基复合材料的研究提供新思路。     

Air route network optimization in fragmented airspace based on cellular automata

Air route network optimization,one of the essential parts of the airspace planning,is an effective way to optimize airspace resources,increase airspace capacity,and alleviate air traffic con gestion.However,little has been done on the optimization of air route network in the fragmented airspace caused by prohibited,restricted,and dangerous areas (PRDs).In this paper,an air route network optimization model is developed with the total operational cost as the objective function while airspace restriction,air route network capacity,and non-straight-line factors (NSLF) are taken as major constraints.A square grid cellular space,Moore neighbors,a fixed boundary,together with a set of rules for solving the route network optimization model are designed based on cellular automata.The empirical traffic of airports with the largest traffic volume in each of the 9 flight information regions in mainland China is collected as the origin-destination (OD) air port pair demands.Based on traffic patterns,the model generates 35 air routes which successfully avoids 144 PRDs.Compared with the current air route network structure,the number of nodes decreases by 41.67％,while the total length of flight segments and air routes drop by 32.03％ and 5.82％ respectively.The NSLF decreases by 5.82％ with changes in the total length of the air route network.More importantly,the total operational cost of the whole network decreases by 6.22％.The computational results show the potential benefits of the model and the advantage of the algorithm.Optimization of air route network can significantly reduce operational cost while ensuring operation safety.     

振动载荷和定应变对HTPB推进剂基体/颗粒粘接界面影响

为研究振动载荷和定应变对HTPB推进剂基体/颗粒粘接界面的影响,进行了振动载荷和定应变作用下HTPB推进剂高温老化试验,测试了不同载荷和老化时间下推进剂的宏观力学性能,利用扫描电镜观测了推进剂的细观破坏过程,基于颗粒增强本构理论,分析了推进剂基体/颗粒粘接界面的损伤规律。结果表明,振动载荷和定应变的作用使HTPB推进剂的初始模量和抗拉强度均减小,高温老化、定应变和振动载荷的作用都会破坏推进剂基体/颗粒粘接界面、降低推进剂固体颗粒模量增强效果,定应变状态下振动载荷作用后,粘接界面损伤最严重。