高温空气传输特性对边界层稳定性及转捩预测的影响

为了研究黏度和导热系数对边界层内基本流和流动稳定性的影响,首先通过分析比较Sutherland公式和目前常用的Gupta等人的拟合关系式,建立了高温气体下黏度和导热系数的计算模型,并分别将Sutherland公式和新建立的计算模型应用于7组元化学平衡流的平板模型,在马赫数为10,16和20,飞行高度为30-5km等条件下分别对黏度和导热系数的模型进行比较.计算结果表明:在高温范围内,黏度和导热系数均影响着边界层的基本流、流动稳定性及转捩预测,且两者影响的趋势相反,黏度的增加、导热系数的减小都能使扰动的增长率变大,增长区变宽,转捩位置提前.      

改进型滑模变结构电机控制的脉振电流注入法研究

为了提高永磁同步电机无位置传感器技术的控制性能,在电机动态品质优化的研究中,以滑模变结构控制器替代传统的PI控制器,采用新型趋近律函数改进滑模控制器的输出模型,削弱了传统滑模控制存在的抖振,提高了控制系统的抗干扰能力。在分析无位置传感器技术时,引入高通谐振滤波器,采用具备以高信噪比为特点的两相静止坐标系下高频脉振电流注入法。仿真结果表明,在带高通谐振滤波器的高频脉振电流注入法中运用滑模变结构控制器,提高了转子位置估计的精度,增强了控制系统的鲁棒性。     

High-Energy Electron Beam Relaxation in a Stationary Plasma Thruster

In the paper, processes of high-energy electron beam interaction with plasma particles in a discharge channel of a stationary plasma thruster are analyzed and the results are presented.     

Hardware reconfiguration algorithm in multiprocessor systems of integrated modular avionics

Reconfiguration of multiprocessor systems makes it possible to improve their failure-resistance that is especially important for the integrated modular avionics systems. The algorithm considered in this paper allows minimizing the reservation and providing the better safety level and more effective flight completion or even its further execution in the case of failures of airborne equipment.     

利用机载GNSS-R的有效波高反演技术

采用自主研发的多源多宿GNSS-R(Global Navigation Satellite System-Reflections,全球导航卫星系统反射信号)海洋环境遥感探测系统,在天津渤海湾特定区域进行了3次机载校飞试验,获得了大量有效GNSS-R信号数据,对自然条件下的海面有效波高进行了反演处理。该系统通过对接收的GNSS直达信号和海面反射信号进行相关运算处理,可以获得DDM(Delay-Doppler Mapping,时延—多普勒映射)图谱,再利用DCF(Derivative of the Correlation Function,相关函数的导数)在DDM图谱基础上进行相关功率波形的计算,进而通过计算DCF的函数波形宽度得到海面有效波高,验证了该方法的可行性。该方法具有全天时、全天候、高分辨率、低成本等优点,对全球范围内中小尺度海洋状态和物理现象的监测具有重要意义。     

航电系统安全性分析工具设计与研究

随着航电系统综合化程度的不断提高,传统的安全性分析方法过于依赖工程经验,难以保证失效模式的完备性。同时在系统迭代设计的过程中,由于系统的复杂性,会导致安全性分析工作量过大,增加了时间及经济成本。针对上述问题,设计了一种自动化安全性分析工具,基于Sys ML描述语言建立安全性数据模型,采用路径追溯的方法完成故障树自动建模,并对生成的故障树进行共模分析和区域安全性分析。以某系统为例的实验结果表明,该工具能够实现故障树自动建模与分析,提高了安全性分析的效率和完备性。     

L波段数字航空通信系统研究

随着全球航空运输的发展,空中交通管制与航空公司运控等航空业务对航空通信系统的数据传输速率、频谱利用率、航空通信网容量等性能提出了更高的要求。虽然现阶段基于甚高频的航空通信系统得到了迅速的发展,但仍受限于标准体制、技术壁垒等因素,难以满足持续增长的运行需求。L波段数字航空通信（L-band digital aeronautical communication system,L-DACS）数据链技术作为新一代航空通信系统的预选方案,是有效解决频谱资源饱和难题、满足高速率传输需求的有效途径。本文在总结L-DACS数据链技术发展现状的基础上,阐述了该通信系统现阶段的技术标准,分析了L-DACS发展所面临的挑战,提出了对应的发展建议,为面向航空宽带通信L-DACS的研究提供了参考与借鉴。     

Modeling of ionospheric scintillation at low-latitude

The presence and movement of plasma density fluctuations in the F-region of the ionosphere are studied by monitoring phase and amplitude of radio waves propagating through the region. In this paper, we have used weak scattering theory and assumed the plasma density fluctuations to behave like phase changing diffraction screen. Appropriate relations for scintillation index S₄, and phase variance δ? are derived and computed for different parameters of the plasma density irregularities of the ionosphere. SROSS-C2 satellite in situ measurements of plasma density fluctuations, which provide direct information about the structure and morphology of irregularities that are responsible for scintillation of radio waves, were used first time to develop a scintillation model for low latitude. It is observed that the scintillation index S₄ and phase variance δ? depends on the strength of the plasma turbulence. Finally, the results obtained from modeling are compared and discussed with the available recent results.     

Evolution of periodic orbits near the Lagrangian point L2

A study of the evolution of the periodic and the quasi-periodic orbits near the Lagrangian point L₂, which is located to the right of the smaller primary on the line joining the primaries and whose distance from the more massive primary is greater than the distance between the primaries, in the framework of restricted three-body problem for the Sun–Jupiter, Earth–Moon (relatively large mass ratio) and Saturn–Titan (relatively small mass ratio) systems is made. Two families of periodic orbits around the smaller primary are identified using the Poincaré surface of section method – family I (initially elliptical, gradually becomes egg-shaped with the increase in the Jacobi constant C and elongated towards the more massive primary) and family II (initially egg-shaped orbits elongated towards L₂ and gradually becomes elliptical with the increase in C). The family I in the Sun–Jupiter and Saturn–Titan systems contains two separatrix caused by third-order and fourth-order resonances, while the Earth–Moon system has only one separatrix which is caused by third-order resonances. Also in the Sun–Jupiter and the Saturn–Titan systems, family I merge with family II, around Jacobian constant 3.0393 and 3.0163, respectively, while in the Earth–Moon system, family II evolves separately from two different branches. The two branches merge at C = 3.184515. In the Earth–Moon system, the family II contains a separatrix due to third-order resonances which is absent in the other two systems.     

Attitude control system of the first Russian nanosatellite <Emphasis Type="Italic">TNS-0 no. 1</Emphasis>

The results of designing the attitude control system of the first Russian nanosatellite TNS-0 no. 1 providing orientation of its longitudinal axis along the local geomagnetic field induction vector are presented. The system consists of a permanent magnet and two sets of hysteresis rods. The magnetic and geometric parameters of the magnet and rods are calculated. The influence of the permanent magnet field on the hysteresis rods and mutual influence of the rods in the case of compact satellite packaging are analyzed. Examples of calculations of transient processes and steady-state angular satellite motion are presented.