MEMS陀螺双通道数字接口系统设计

针对现有的MEMS陀螺接口系统只能对一个陀螺进行测控导致标定测控效率低下的问题,提出了一种新型的可同时对两个陀螺进行测控的MEMS陀螺双通道接口系统架构,并设计了一套与之对应的MEMS陀螺双通道测控电路,包括前端模拟电路、后端数字系统和人机交互终端。通过设计的人机交互系统对整个系统的全部功能进行了测试,其中扫频、锁相、稳幅、线性度和零偏稳定性等功能均能正常运行,在实际使用测试中相较于单通道接口系统测控效率提升到2倍以上。     

基于非全向天线的无人机MIMO信道模型研究

为研究无人机信道特性,针对地面控制站( GCS)环境特点和非全向多天线系统,建立并分析了基于散射体三维几何分布的单跳同心圆筒散射(GBSBCCS)宽带传播模型,根据方位角非全向散射和俯仰角非对称分布的特性,结合无人机实际飞行参数特点,推导出简洁的空时频联合相关函数.通过仿真进行了验证,并对相关特性影响因素进行分析,结果...     

小型遥测系统的容量和信道设计

论述了某型号无人机遥测系统中的容量和信道设计问题.文中对该遥测系统的组成和原理进行了介绍.结合具体的遥测任务需求,在容量设计中确定了数据传输率和使用的帧格式,在信道设计中,通过计算实际信道中的误码率,提出了相应的信道编码方案以确保数据传输的低误码率要求.     

简单快速的平面散乱点集凸包算法

凸包问题是计算几何的基本问题之一,在许多领域均有应用,传统点集凸包算法和简单多边形凸起算法平行发展,互不相干,文中将简单多边形凸包算法应用用于散乱点集凸包问题中,提出了新的点集凸包算法,新算法不仅达到了Ｏ（ｎｌｏｇｎ）的理论时间复杂度下限,而且极其简单,易于实现,该算法已应用于工厂设计软件ＰＤＳＯＦＴ中,实践证明效果很好。     

基于NIRGAM的片上网络性能仿真

采用虫孔交换和虚拟通道技术的片上网络系统(NoC)能极大地降低传输延时,防止微片拥塞,增大网络吞吐率,从体系结构上解决了总线通信技术的瓶颈。片上网络的虚拟通道由多个缓冲区组成,其数目直接影响芯片的面积,必须通过仿真得到面积和缓冲区数目的平衡。使用NIRGAM仿真器对不同缓冲区数目的 2D Mesh片上网络进行了仿真,对其源代码中几个重要参数提出了修改建议,仿真结果表明,在本文配置的通信情况下缓冲区深度为4微片时NoC系统整体性能最好。     

不可微多目标凸规划的对偶理论

本文建立了不可微多目标凸规划的一种形式的对偶规划,讨论了关于真有效解的直接对偶定理、逆对偶定理和弱对偶定理的对偶结果。     

一种新的广义凸多目标分式规划的对偶定理

本文给出了一类新的广义凸函数-(F,α,ρ,θ)-b-凸函数,讨论了多目标分式规划(MFP)的三种对偶模型:Mond-Weir型对偶、Lagrange型对偶、Schaible型对偶,并基于(F,α,ρ,θ)-b-凸性证明了各自相应的弱、强对偶定理。     

Numerical investigation on flow mechanism in a supersonic fluidic oscillator

A type of supersonic fluidic oscillator is proposed and its ability to generate pulsating supersonic jet is proved in this paper. Unsteady two-dimensional numerical simulations reveal that the fluid transforms from subsonic to supersonic condition in the mixing chamber of oscillator after the supplied flow pressure increases from 1.1 × 10⁵ Pa to 5.0 × 10⁵ Pa. When the supersonic flow is formed inside the oscillator, the wall-attached flow represents expansion wave and compression wave alternately. The oscillating frequency will saturate to a certain value with the increase of supplied pressure. Examination of the internal fluid dynamics indicates that the flow direction inside the FeedBack Channel (FBC) is related to the change of the local pressure at the inlet and the outlet of the feedback channel. The vortices produced in the mixing chamber present different distribution characteristics with the change of the fluid’s direction in the FBC. The sweeping jet is divided into two jets with varying flow rate over time by the splitter. In the end of two channels, two jets are accelerated above sound speed by convergent-divergent nozzle. Therefore, pulsating supersonic jets are produced at two outlets for this type of fluidic oscillator.     

频率选择性衰落信道DS-CDMA无人机中继通信系统航迹规划

无人机中继通信是实现远距离无线通信的一种重要技术手段，无人机的飞行航迹对无人机中继通信系统的链路传输可靠性存在显著的影响，在频率选择性衰落信道环境下研究了基于直序列码分多址（DS-CDMA）的无人机中继通信系统的航迹优化的问题。首先，给出了基于DS-CDMA的译码转发无人机中继通信系统的模型，并理论分析给出无人机中继通信系统的链路中断概率及平均误码率计算公式，以此为基础，基于链路中断概率最小化准则提出了中继无人机的航迹规划方法，最后通过仿真验证了所提出方法的正确性与有效性。研究表明：最大比值合并DS-CDMA无人机中继通信系统可充分获取频率选择性衰落信道提供的分集增益，显著改善链路传输的可靠性。     

Development of secondary flow field under rotating condition in a straight channel with square cross-section

The developing secondary flow fields in the entrance section of a rotating straight channel were experimentally investigated using Particle Image Velocimetry (PIV). The effects of streamwise position, Reynolds number and rotation number on the development of the secondary flow fields were revealed. The results show that the absolute values of vorticity flux of the trailing side roll cells increase with increasing radius of the measured plane and rotation number. When the absolute value of vorticity flux exceeds a critical value, the merging of the trailing side roll cells appears. Moreover, when the number of the trailing side vortex pairs is even, the absolute values of vorticity flux of the leading side vortices increase along streamwise direction. Otherwise, the absolute values decrease along the streamwise direction. By the circulation analysis, this phenomenon was found to have relationship with the merging of the trailing side roll cells, and further concluded that the secondary flow field in a rotating channel has to be treated as a whole. At last, the increase of the Reynolds number was found to be able to induce the merging position moves upstream.