立方体星的技术发展和应用前景

系统论述了立方体星技术发展的三个阶段;从2010-2013年已成功发射的立方体星与纳卫星中挑选了10颗典型卫星,研究分析其技术水平、应用价值和特点优势;并重点论述了立方体纳卫星的应用;最后预测了立方体纳卫星的未来应用前景。     

A strategic flight conflict avoidance approach based on a memetic algorithm

Conflict avoidance （CA） plays a crucial role in guaranteeing the airspace safety. The cur- rent approaches, mostly focusing on a short-term situation which eliminates conflicts via local adjust- ment, cannot provide a global solution. Recently, long-term conflict avoidance approaches, which are proposed to provide solutions via strategically planning traffic flow from a global view, have attracted more attentions. With consideration of the situation in China, there are thousands of flights per day and the air route network is large and complex, which makes the long-term problem to be a large-scale combinatorial optimization problem with complex constraints. To minimize the risk of premature convergence being faced by current approaches and obtain higher quality solutions, in this work, we present an effective strategic framework based on a memetic algorithm （MA）, which can markedly improve search capability via a combination of population-based global search and local improve- ments made by individuals. In addition, a specially designed local search operator and an adaptive local search frequency strategy are proposed to improve the solution quality. Furthermore, a fast genetic algorithm （GA） is presented as the global optimization method. Empirical studies using real traffic data of the Chinese air route network and daily flight plans show that our approach outper- formed the existing approaches including the GA .based approach and the cooperative coevolution based approach as well as some well-known memetic algorithm based approaches.     

吊挂系统对波瓣混合排气系统气动热力性能影响

为了明确短舱中吊挂系统的堵塞效应对波瓣混合排气系统气动热力性能的影响,采用数值模拟的方法对包含吊挂的混合排气系统进行了定量研究。研究结果表明,受吊挂系统的影响,在波瓣混合排气系统混合段内,存在着一大尺度的回流区,其作用范围随吊挂长度的增加而增加。在性能参数方面,与未考虑吊挂系统时相比,考虑吊挂之后,虽然混合排气系统出口处热混合效率以及推力系数下降很小,最大降幅仅分别为0.017和0.01,但总压恢复系数却显著下降,最大降幅达到了0.03。此外,随着吊挂系统长度的变化,排气系统出口处的热混合效率、总压恢复系数以及推力系数变化幅度小于0.01,变化很小。     

Optimization of beamforming and path planning for UAV-assisted wireless relay networks

Recently, unmanned aerial vehicles （UAVs） acting as relay platforms have attracted considerable attention due to the advantages of extending coverage and improving connectivity for long-range communications. Specifically, in the scenario where the access point （AP） is mobile, a UAV needs to find an efficient path to guarantee the connectivity of the relay link. Motivated by this fact, this paper proposes an optimal design for beamforming （BF） and UAV path planning. First of all, we study a dual-hop amplify-and-forward （AF） wireless relay network, in which a UAV is used as relay between a mobile AP and a fixed base station （BS）. In the network, both of the AP and the BS are equipped with multiple antennas, whereas the UAV has a single antenna. Then, we obtain the output signal~to-noise ratio （SNR） of the dual-hop relay network. Based on the criterion of maximizing the output SNR, we develop an optimal design to obtain the solution of the optimal BF weight vector and the UAV heading angle. Next, we derive the closed-form outage probability （OP） expression to investigate the performance of the dual-hop relay network conveniently. Finally, computer simulations show that the proposed approach can obtain nearly optimal flying path and OP performance, indicating the effectiveness of the proposed algorithm. Furthermore, we find that increasing the antenna number at the BS or the maximal heading angle can significantly improve the performance of the considered relay network.     

超燃冲压发动机旋转斜坡概念研究

基于斜坡增强混合及旋转冲压的设计思想,提出一种旋转斜坡概念,即通过斜坡旋转产生大尺度旋涡及旋转运动激波来增强混合。采用Fluent软件求解URANS方程,对旋转斜坡非定常流场开展了数值模拟研究,分析了斜坡旋转速度对燃烧室的流场特征、涡量、总压损失等性能的影响。结果表明斜坡旋转促进了凹腔剪切层的振荡,并在凹腔内形成了较强烈的流向旋涡。当旋转速度54.3r/min时,斜坡旋转导致的流向涡量峰值约是无旋状态下的4倍左右,总压恢复系数比斜坡静止状态最大降低约10%。     

基于模块度的复杂网络社团结构聚类新算法

针对传统的分裂聚类算法删除连边会影响节点划分的问题,结合K-means算法的思想并加以改进,提出了一种以邻居节点为聚类备选集,所有社团中心节点同时聚类的同步聚类算法。该算法根据节点中心度和最短路变化率确定社团中心节点集,然后以中心节点为社团中心,以邻居节点为聚类备选集合进行聚类,完成社团的划分。将算法应用到Zachary网络中并与GN算法、Top Leader算法进行比较,仿真结果表明该算法对网络有较好的划分。     

椭圆形切扇修形对波瓣混合器掺混性能影响

在保证面积不变的情况下,选取不同的长轴、短轴,对波瓣混合器进行椭圆形切扇修形,研究切口深度与宽度对波瓣混合器掺混性能的影响规律。使用商用 CFD 软件对流场进行数值模拟。结果显示,对波瓣侧壁进行切扇处理会加强流向涡的强度,切扇越深,流向涡强度越大;切扇波瓣流向涡的耗散速率要大于基准波瓣混合器的流向涡耗散速率,预示着更为高效的掺混;引射系数与切口深度成正比,而总压恢复系数与切口深度成反比。考察了两种衡量热混合效率的模型并对其信度进行了比较,发现在 x =0.4 m 之前切扇可以提高热混合效率,而在 x =0.4 m 之后,基准波瓣混合器热混合效率要大于切扇波瓣混合器。     

无线传感器网络时间同步协议动态切换机制

针对当前无线传感器网络时间同步协议通用性差的问题,提出了基于主动编程思想的时间同步协议动态切换机制,设计了能够动态适配的时间同步协议切换框架,重点讨论了节点间相互通信、时间戳标记、协议切换、本地时间与全局时间的转换等4个关键问题,并且在TinyOS（Tiny Operating System,微操作系统）平台上对新机制进行了仿真验证,比较了新机制同2种主流时间同步协议之间的性能差异.仿真结果表明：新机制能实现时间同步协议的动态配置,提高协同效率,节省切换开销,具有良好的应用前景.     

基于BP网络的机组工作量评估方法研究

为研究机组工作量的评估问题,搭建了模拟飞行实验平台,设定了7种不同负荷的飞行任务。模拟飞行中,对被试的生理指标进行测量,并采集其主观评价值。采用BP网络进行数学建模,将生理指标测量值作为输入、NASA-TLX表法的评价值作为输出,利用输入、输出模式对对网络进行训练,并对该方法进行验证。结果表明,基于BP网络的机组工作量评估方法,较传统方法更为稳定、精确,且大大降低了被试数量。提高训练模式对的数量、简化生理指标的测量过程,并保证测量精度是该方法成功的关键。     

序言CSCD

北斗全球卫星导航系统的建成、应用奠定了我国自主时空信息服务基础,随之我国进入综合PNT体系发展建设新阶段。综合PNT体系将以北斗系统为核A通过多类PNT技术手段协同与融合应用,实现更为精准、泛在和智能的PNT服务能力。通导一体化作为综合PNT核心手段之一,得益于通信极其广泛的覆盖性及日益增强的信息传输能力,依托通信网络对卫星导航系统进行补充、备份和增强,展现出显著的协同优势,因此也成为了领域研究的热点方向。