Use of land＇s cooperative object to estimate UAV＇s pose for autonomous landing

The research of unmanned aerial vehicles＇（UAVs＇）autonomy navigation and landing guidance with computer vision has important signifcance.However,because of the image blurring,the position of the cooperative points cannot be obtained accurately,and the pose estimation algorithms based on the feature points have low precision.In this research,the pose estimation algorithm of UAV is proposed based on feature lines of the cooperative object for autonomous landing.This method uses the actual shape of the cooperative-target on ground and the principle of vanishing line.Roll angle is calculated from the vanishing line.Yaw angle is calculated from the location of the target in the image.Finally,the remaining extrinsic parameters are calculated by the coordinates transformation.Experimental results show that the pose estimation algorithm based on line feature has a higher precision and is more reliable than the pose estimation algorithm based on points feature.Moreover,the error of the algorithm we proposed is small enough when the UAV is near to the landing strip,and it can meet the basic requirements of UAV＇s autonomous landing.     

铸铝薄壁件数控加工变形控制

为了解决铸铝薄壁件在加工过程中切削力及初始进刀带来的影响,针对此类零件的加工工艺进行研究,从零件材料性能,工艺方法、进退刀方式、切削参数等方面进行深入分析与应用,采取减小切削量增大进给值的方法及圆插补和斜坡进刀方式控制切削变形,利用压顶交叉的方式控制装夹变形,提高了零件加工的可靠性,保证了零件精确尺寸。     

一种CCSDS深空标准的LDPC码高效实现

针对CCSDS(空间数据系统咨询委员会)深空通信标准LDPC(低密度奇偶校验码),为减少定点量化后的译码性能损失,提出了一种改进的译码修正算法。通过分析矩阵结构特点,并引入交错译码结构以及流水结构,设计了一种适合该标准深空通信LDPC码编译码器的高效实现结构。使用此结构,在Xilinx公司的XC5VSX95T芯片上实现了CCSDS深空通信标准的(8 192,4 096)LDPC码,在40次迭代情况下可以达到47m的吞吐率。实践表明:该设计可以灵活地移植应用于其他码率的CCSDS深空通信标准LDPC编译码器设计。     

Performance simulation of high altitude scientific balloons

The design and operation of a high altitude scientific balloon requires adequate knowledge of the thermal characteristics of the balloon to make it safe and reliable. The thermal models and dynamic models of altitude scientific balloons are established in this paper. Based on the models, a simulation program is developed. The thermal performances of a super pressure balloon are simulated. The influence of film radiation property and clouds on balloon thermal behaviors is discussed in detail. The results are helpful for the design and operate of safe and reliable high altitude scientific balloons.     

航空自组网STDMA时隙分配算法的设计与实现

航空自组网(AANET)是一种节点高速运动、网络拓扑持续快速变化的新型自组织网络。针对AANET的特点,提出了一种新的时分多址(TDMA)时隙分配方法。首先,根据高动态航空网络环境中媒体访问控制(MAC)协议的特点,推导出可以共用一个时隙进行通信的连接集合的计算方法,并建立了面向连接的空间复用TDMA(STDMA)时隙分配优化数学模型。然后,提出一种分布式STDMA时隙分配算法IDTA。IDTA不需要中心节点收集网络信息,分为2个同步的进程在发送节点和接收节点同时运行,而且能够根据连接的优先级按需分配时隙。最后,在OMNeT++仿真平台上建立计算机仿真模型,仿真结果显示:IDTA比其他分布式STDMA时隙分配算法更加适用于高动态的航空网络环境。     

基于遗传算法的飞机经济爬升速度优化方法

为提高宽体飞机的爬升经济性,首先建立了爬升阶段飞行动力学模型和优化目标计算模型,确定了基于速度优化的最佳爬升策略;然后,在最佳爬升策略的基础上,建立了基于遗传算法的双表速爬升优化模型,得到近似最佳爬升策略,并分析了该爬升策略的可行性;最后,以某宽体飞机为例,分析了近似最佳爬升策略的影响因素。研究结果表明:最佳爬升策略相对传统爬升策略经济性提升3%~8%,且改进后的近似爬升策略与最佳爬升策略误差不超过1.4%;飞机重量、温度偏差和成本指数均会影响爬升策略的性能参数。     

三维翼面结冰过程及其影响数值研究

为得到三维机翼及翼身尾构型在结冰条件大气中的结冰过程和影响,采用结构化网格对M6机翼和翼身尾构结冰过程进行数值模拟,对飞机结冰过程的数值模拟采用欧拉两相流法求解水滴撞击特性,基于Messinger热力学模型模拟冰形增长过程,对其水滴撞击特性、结冰形状及结冰后对气动特性影响进行研究.分析结果可得:机翼展向,随着弦长变小,结冰量逐渐增多,尤其对大展弦比机翼更为明显.同时机身前端迎风面也是比较容易积冰的区域.     

Thermal shock damage behavior of CVD ZnS by oxygen propane flame：A numerical and experimental study

Chemical vapor deposition zinc sulfide （CVD ZnS） is widely used as an infrared window material to transmit infrared signals, keep the aerodynamic shape and protect its imaging system, which often suffers high temperature and complicated thermal stresses. The purpose of this paper is to investigate the thermal shock damage of CVD ZnS through a finite element method and oxygen propane flame experiments. The finite element model is developed to simulate the temperature and thermal stress fields by an oxygen propane flame. Then, the thermal shock experiments are performed to investigate the thermal shock damage behavior. The results show that the temperature rising rate of the shock surface is fast during the initial heating stage resulting in high thermal stress. After the thermal shock experiment, the scanning electron microscope （SEM） photographs shows that the shock surface of the specimen becomes rough and the microcracks occur in the thermal shock zone. Good agreements are achieved between the numerical solutions and the experimental results.     

卫星测控直扩信号安全性能评价体系研究

为了定量评估直扩信号的安全性能,在给出卫星测控直扩信号安全防护定义的基础上,对卫星测控直扩信号安全性能评价指标进行了研究.在深入分析直扩信号典型威胁的基础上,提出了等效码长、调制指数、码速率截获因数、等效码长截获因数、码序列截获因数、干扰因数等衍生指标,分析、仿真了它们的影响因素,得到了它们与基本指标的关系,初步建立了直扩信号安全性能评价体系,为后续安全性能评估打下基础.