基于有向图的蜂群无人机故障影响

基于蜂群无人机控制模型，针对虚假数据注入的故障情形，为了分析该故障情形下，蜂群无人机中故障的的影响及传播关系，采用故障传播有向图及一致性理论，开展蜂群无人机故障影响机理研究。首先，通过Dijkstra算法计算故障源到各无人机的最短路径，建立故障传播有向图；然后预测各无人机受故障影响的程度，结合蜂群无人机系统，计算一致性行为偏差的指标，并将其作为实际故障影响程度；最后，通过对预测结果与实际故障影响程度进行仿真比较，验证了所建立的故障影响机理的合理性。     

Effect of biases in integrity monitoring for RTK positioning

In road transport, continuous high-accuracy positioning is required in real time. To ensure the proper functioning and safety of vehicular applications, integrity monitoring (IM) is needed to protect from the positioning errors under a certain alert limit (AL) with a pre-defined probability of misleading information (MI). In this study, a detailed threat model is developed for real-time kinematic (RTK) positioning application of short baselines. The model distinguishes between ambiguity-float and -fixed scenarios, and considers the influences of phase and code multipath as well as between-receiver atmospheric residuals. With the float ambiguities temporally constrained, the bias contribution that propagates with time-updated ambiguities was studied analytically for the horizontal protection level (HPL) in IM. Based on real data from both static and kinematic experiments, HPL was computed along the direction of the semi-major axis of the horizontal error ellipse. In ambiguity-float and -fixed cases, the HPL was mostly several meters and decimetres, respectively. It was found that time-propagated biases play a dominant role in the ambiguity-float HPL, and among them, phase and code multipath had in general the largest contributions. For ambiguity-fixed case, the phase multipath was found to play a dominant role in the HPL. This shows the importance of considering the biases in the RTK IM for both the ambiguity-float and -fixed scenarios. Given a horizontal alert limit (HAL) of 5 m, the availabilities of ambiguity-float solutions were low, i.e., below 50% for the static roof tests and below 5% for the kinematic road tests. For the ambiguity-fixed scenario, with HAL at 0.5 m, integrity availability was nearly 100% for the static roof tests and above 85% for the kinematic road tests.     

Three-Dimentional Surface Light Irradiance Reconstruction in Bioluminescence Tomography

Reconstruction of 3D surface irradiance distribution using multiple views captured by charged coupled device(CCD)camera is the basis of solving the light source in bioluminescence tomography(BLT).A simple and convenient mapping technique based on the pin-hole imaging model and Lambert′s cosine law was presented to establish the relationship between gray levels and irradiance intensities.Compared with previous integrating sphere camera calibration used in BLT,the proposed method can effectively avoid heavy burden of simulation experiment to obtain the corresponding relationship of gray levels and irradiance intensities.The accuracy and feasibility of the proposed method are validated with no more than 1mm location error by different types of phantom experiments.The mapping approach is also applicable to other noncontact optical imaging system.     

Crack monitoring method based on Cu coating sensor and electrical potential technique for metal structure

Advanced crack monitoring technique is the cornerstone of aircraft structural health monitoring.To achieve real-time crack monitoring of aircraft metal structures in the course of service,a new crack monitoring method is proposed based on Cu coating sensor and electrical potential difference principle.Firstly,insulation treatment process was used to prepare a dielectric layer on structural substrate,such as an anodizing layer on 2A12-T4 aluminum alloy substrate,and then a Cu coating crack monitoring sensor was deposited on the structure fatigue critical parts by pulsed bias arc ion plating technology.Secondly,the damage consistency of the Cu coating sensor and2A12-T4 aluminum alloy substrate was investigated by static tensile experiment and fatigue test.The results show that strain values of the coating sensor and the 2A12-T4 aluminum alloy substrate measured by strain gauges are highly coincident in static tensile experiment and the sensor has excellent fatigue damage consistency with the substrate.Thirdly,the fatigue performance discrepancy between samples with the coating sensor and original samples was investigated.The result shows that there is no obvious negative influence on the fatigue performance of the 2A12-T4 aluminum alloy after preparing the Cu coating sensor on its surface.Finally,crack monitoring experiment was carried out with the Cu coating sensor.The experimental results indicate that the sensor is sensitive to crack,and crack origination and propagation can be monitored effectively through analyzing the change of electrical potential values of the coating sensor.     

Network analysis of Chinese air transport delay propagation

The Chinese air transport system has witnessed an important evolution in the last dec-ade, with a strong increase in the number of flights operated and a consequent reduction of their punctuality. In this contribution, we propose modelling the process of delay propagation by using complex networks, in which nodes are associated to airports, and links between pairs of them are assigned when a delay propagation is detected. Delay time series are analysed through the well-known Granger Causality, which allows detecting if one time series is causing the dynamics observed in a second one. Results indicate that delays are mostly propagated from small and regio-nal airports, and through flights operated by turbo-prop aircraft. These insights can be used to design strategies for delay propagation dampening, as for instance by including small airports into the system's Collaborative Decision Making.     

复杂目标GRECO方法的分屏显示计算

图形电磁计算(GRECO)是一种计算复杂目标雷达散射截面(RCS)的有效方法,但必须先有一个易于提取外形参数的数据文件.基于GRECO法,针对用各种通用商业软件造型生成的模型文件,利用商业软件Rhino进行转化,生成适于RCS计算的数据文件,这种处理数据的方法具有广泛的适用性,且不会丢失任何局部细节.通过分屏显示计算方法,提高了对电大尺寸目标的计算精度;采用OpenGL的显示列表技术使得程序运行花费较少的时间.结合GRECO的特点,提出了一种分析目标散射源的简便的方法,便于分析目标的雷达散射截面特性.结果表明,本方法与面劈法的计算结果吻合较好,具有较好的工程应用价值.     

Satellite collision probability estimation using polynomial chaos expansions

This paper presents the application of polynomial chaos (PC) to estimating the probability of collision between two spacecraft. Common methods of quantifying this probability for conjunction assessment use either Monte Carlo analyses or include simplifying assumptions to improve tractability. A PC expansion, or PCE, provides a means for approximating the solution to a large set of stochastic ordinary differential equations, which includes orbit propagation. When compared to Monte Carlo methods, non-intrusive, i.e., sampling-based, PCE generation techniques may greatly reduce the number of orbit propagations required to approximate the possibly non-Gaussian, a posteriori probability density function. The presented PC-based method of computing collision probability requires no fundamental simplifying assumptions, and reduces the computation time compared to Monte Carlo. This paper considers two cases where the common conjunction assessment assumptions are no longer valid. The results indeed demonstrate a reduction in computation time when compared to Monte Carlo, and improved accuracy when compared to simplified techniques.     

固体推进剂复合型裂纹扩展数值计算

用粘弹性有限元法,分别以尖角形、椭圆形、圆形裂尖反映裂尖的变形,以最大周向应力准则和最大能量释放率准则作为裂纹扩展方向的判断依据,以J积分作为裂纹扩展的起始判据,计算了不同倾斜角裂纹的初始扩展方向.采用多个扩展步递增循环计算的方法,得到了不同倾斜角裂纹的扩展路径,并在扩展路径上设置粘结损伤单元,模拟了裂纹的动态扩展过程...     

基于自适应仿射传播聚类的雷达信号分选方法

复杂体制的雷达不断应用于实际,使得基于到达时间单参数的雷达信号分选方法遇到了技术瓶颈.然而,基于多参数的信号分选方法,如K-均值聚类和模糊函数C均值聚类,前者对初始类中心敏感、需预知聚类数,后者对类隶属度的选取、相似度矩阵的建立存在不确定性,使得这些方法在自适应雷达信号分选中受到了限制.自适应仿射传播聚类不仅可以克服上...     

光学头罩超声速绕流流场光学传输效应风洞试验研究

在Ma=3连续超声速风洞中,开展了光学头罩绕流流场光学传输效应的风洞模拟试验方法研究,进行了现场振动测量与隔离,研制了专用试验装置,采用哈特曼传感器和剪切干涉仪两种手段进行了光学传输效应的试验测量。试验中,针对试验装置各部分的不同组合状态,进行了大量的测试,研究了试验装置有效性以及试验数据重复性,着重分析了探测光束的PV值与RMS值。结果表明：导流板可明显抑制风洞洞壁边界层干扰,试验装置与方法可行,对于连续式风洞中模型绕流流场光学传输效应测试有一定参考价值。