基于听觉感知的驾驶舱信息提示设计研究

为研究飞机驾驶舱中不同的听觉信息提示方式对感知效率、关注程度影响差异,基于飞行仿真场景构建飞行任务,在任务执行中提供听觉刺激提示,采集被试任务全过程中的脑电信号并进行了时域和频域维度的分析,对比语言听觉/非语言听觉以及不同播报速度的工效影响,总结了被试对驾驶舱听觉信息提示的反应特征,为听觉信息提示的人机交互设计提供参考建议.     

涡轮基组合循环发动机分布式控制系统通信网络混合拓扑结构优化方法

涡轮机组合循环(Turbine based combined cycle,TBCC)发动机控制系统通信网络拓扑结构是其分布式控制系统方案设计的重要部分,优化网络拓扑结构可提高发动机推重比和控制系统可靠性。本文基于智能优化算法提出TBCC分布式控制系统网络拓扑结构优化方法。基于图论建立TBCC几何模型和网格模型,以重量和可靠性为优化性能指标,同时考虑发动机表面高温区域以及控制节点的工作可靠性,分别采用粒子群算法和遗传算法优化星形结构中智能中央节点位置、中央节点的环形拓扑结构,获得星形-环形混合拓扑结构。仿真实例表明,基于本文方法优化所得的混合拓扑结构相较于星形集中式控制结构,系统重量降低了51.9%。     

Evaluation of SARAL/AltiKa performance using GNSS/IMU equipped buoy in Sajafi,Imam Hassan and Kangan Ports

Performance of SARAL/AltiKa mission has been evaluated within 2016 altimeter calibration/validation framework in Persian Gulf through three campaigns conducted in the offshore waters of Sajafi, Imam Hassan and Kangan Ports, while the altimeter overflew the passes 470, 111 and 25 on 13 Feb, 7 March and 17 June 2016, respectively. As the preparation, a lightweight buoy was equipped with a GNSS receiver/choke-ring antenna and a MEMS-based IMU to measure independent datasets in the field operations. To obtain accurate sea surface height (SSH) time series, the offset of the onboard antenna from the equilibrium sea level was predetermined through surveying operations as the buoy was deploying in the onshore waters of Kangan Port. Accordingly, the double-difference carrier phase observations have been processed via the Bernese GPS Software v. 5.0 so as to provide the GNSS-derived time series at the comparison points of the calibration campaigns, once the disturbing effects due to the platform tilt and heave have been eliminated. Owing to comparing of the SSH time series and the associating altimetry 1?Hz GDR-T datasets, the calibration/validation of the SARAL/AltiKa has been performed in the both cases of radiometer and ECMWF wet troposphere corrections so as to identify potential land contamination. An agreement of the present findings in comparison with those attained in other international calibrations sites confirms the promising feasibility of Persian Gulf as a new dedicated site for calibration/validation of ongoing and future altimetry missions.     

航天器视场遮挡分析方法研究

敏感器视场遮挡分析是航天器构型布局设计的重要组成部分，针对大型在轨变构型航天器敏感器视场遮挡分析工作量大、出错率高、遮挡率无法量化等特点，本文提出一种基于敏感器第一视角的视场遮挡快速分析方法。该方法通过设置第一视角图像蒙版及图像映射，模拟方锥形、圆锥形、球形等各类敏感器视场，通过逐个像素比对，计算视场遮挡率和遮挡方位。使用此方法建立了空间站敏感器视场遮挡分析系统，结果表明新方法能够显著提高视场遮挡分析效率和准确率，并且为机构类部件运动过程对敏感器视场遮挡的分析提供了有效工具。     

Comparison of GPS derived TEC with the TEC predicted by IRI 2012 model in the southern Equatorial Ionization Anomaly crest within the Eastern Africa region

We have compared the TEC obtained from the IRI-2012 model with the GPS derived TEC data recorded within southern crest of the EIA in the Eastern Africa region using the monthly means of the 5 international quiet days for equinoxes and solstices months for the period of 2012 – 2013. GPS-derived TEC data have been obtained from the Africa array and IGS network of ground based dual-frequency GPS receivers from four stations (Kigali (1.95°S, 30.09°E; Geom. Lat. 11.63°S), Malindi (2.99°S, 40.19°E; Geom. Lat. 12.42°S), Mbarara (0.60°S, 30.74°E; Geom. Lat. 10.22°S) and Nairobi (1.22°S, 36.89°E; Geom. Lat. 10.69°S)) located within the EIA crest in this region. All the three options for topside Ne of IRI-2012 model and ABT-2009 for bottomside thickness have been used to compute the IRI TEC. Also URSI coefficients were considered in this study. These results are compared with the TEC estimated from GPS measurements. Correlation Coefficients between the two sets of data, the Root-Mean Square Errors (RMSE) of the IRI-TEC from the GPS-TEC, and the percentage RMSE of the IRI-TEC from the GPS-TEC have been computed. Our general results show that IRI-2012 model with all three options overestimates the GPS-TEC for all seasons and at all stations, and IRI-2001 overestimates GPS-TEC more compared with other options. IRI-Neq and IRI-01-corr are closely matching in most of the time. The observation also shows that, GPS TEC are underestimated by TEC from IRI model during noon hours, especially during equinoctial months. Further, GPS-TEC values and IRI-TEC values using all the three topside Ne options show very good correlation (above 0.8). On the other hand, the TEC using IRI-Neq and IRI-01- corr had smaller deviations from the GPS-TEC compared to the IRI-2001.     

叶片飞脱下转子动力学响应实验

为了研究大涵道比涡扇发动机叶片飞脱时动力学响应,更好地进行发动机安全性设计,根据相似理论设计了包含叶片飞脱装置的突加不平衡实验系统并进行了实验验证。研究结果表明:设计的突加不平衡实验系统,与某型验证机相似度高,代表性强,能够有效可控地进行突加不平衡实验,重复性好,机理清晰且飞脱不平衡量大,能够真实地模拟发动机叶片飞脱响应。通过实验发现,当大突加不平衡发生时,频谱出现超次谐波并且冲击系数由于挤压油膜阻尼器限幅作用并不呈现线性关系,因而在后续研究中还应注意限幅导致的碰摩问题。      

300 MVA脉冲发电机组滑差方式起动过程研究

介绍了300 MVA脉冲发电机组的滑差装置。对机组采取滑差方式的起动过程进行了分析和等效建模。根据机组实际起动过程电气波形,利用非线性规划模型,建立了滑差装置液体电阻等效仿真模型,并代入机组参数对起动过程进行仿真,仿真结果和实际波形吻合,验证了模型的正确性。在此基础上,为了使机组的转速达到额定转速,提出在滑差装置液体电阻低位时并入两级固体金属电阻后短接的方案,给出了两级固体金属电阻的阻值等理论参数,并通过仿真验证了方案的可行性。建立的仿真模型可以作为研究不同参数、不同控制策略下的机组起动过程动态特性的重要工具。     

在片校准标准件基底边界条件影响

通过分析国内外校准标准件物理边界条件，研究不同校准基底的物理边界条件对共面波导（CPW）传输线特性和校准准确度的影响。研制了W波段砷化镓衬底的多线TRL在片校准标准件，将在片校准标准件分别放置在金属卡盘、玻璃片、吸波材料三种校准基底上。用三种不同校准基底的校准标准件对试验装置校准后，分别提取了CPW传输线的衰减常数、相对介电常数和特征阻抗，并对商用校准标准件104-783A的短路标准和传输线标准进行了测试，验证了结果的合理性。     

Optimization of bits allocation and path planning with trajectory constraint in UAV-enabled mobile edge computing system

In this paper, an Unmanned Aerial Vehicle (UAV) enabled Mobile Edge Computing (MEC) system is studied, in which UAV acts as server to offer computing offloading service to the Mobile Users (MUs) with limited computing capability and energy budget. We aim to minimize the total energy consumption of MUs by jointly optimizing the bit allocation for uplink, computing at the UAV and downlink, along with the UAV trajectory in a unified framework. To this end, a trajectory constraint model is employed to avoid sudden changes of velocity and acceleration during flying. Due to high-order information in use, we lead to a more reasonable nonconvex optimization problem than prior arts. An Alternating Direction Method of Multipliers (ADMM) method is introduced to solve the optimization problem, which is decomposed into a set of easy sub-problems, to meet the requirement on the efficiency in edge computing. Numerical results demonstrate that our approach leads a smoother UAV trajectory, significantly save the energy consumption for UAV during flying.     

Alfvén gravity waves in viscous solar plasma: Effect of the background flow

We study the Propagation and damping properties of Alfvén gravity waves in the presence of the vertical magnetic field in the viscous solar plasma under influence of the background flow by deriving a fourth order dispersion relation in terms of the Doppler shifted frequency. We derive the dispersion relation under WKB and Boussinesq approximation. We study the damping of Alfvén gravity waves for the wave frequencies less than and greater than the Brunt-Väisälä frequency. We find that the Brunt-Väisälä frequency divides the frequency ranges where the weakly or strongly damped oscillations occur. The background flow exhibits a strong effect on weakly damped oscillations and a weak effect on the strongly damped oscillations. We also notice that the damping of both the strong and weakly damped oscillations depend on the Brunt-Väisälä frequency and wave number. The effect of the background flow is also being governed by the Brunt-Väisälä frequency and wave number. We also study the properties of gravity wave mode after filtering the Alfvén wave mode by minimizing the magnetic field and noticed that the background flow shows a very strong effect on the gravity wave mode.