基于实测数据的复合材料构件装配干涉与间隙计算

针对因成型误差引起的复合材料构件装配干涉问题,本文基于激光测量设备获取装配件点云数据,提出一种基于实测数据的复合材料构件装配干涉与间隙的降维求解方法,将三维装配的干涉与间隙计算转化为二维边界距离计算。以某型飞机雷达罩装配为例,通过实验验证了本文所提出的方法与算法的可行性,相较于原有装配工艺,装配精度与装配效率得到了提升。     

基于Kinect三维重建的地下井室可视化方法研究

针对现有地下井室病害探测与维护方法的不足,提出了一种基于Kinect三维重建的地下井室可视化方法,以实现其三维可视化探测与维护.还提出了一种基于多项式曲面拟合的Kinect深度测量误差修正方法,利用联合双边滤波算法对深度图像数据进行预处理;结合SIFT特征匹配和改进的RANSAC算法获取相邻点云间的初始位姿,并利用基于...     

概念设计阶段起落架接地点设计

针对现代民用飞机设计特点,尤其是某些新技术的应用和飞机系列化发展的需求,在充分吸收和借鉴传统飞机概念设计阶段起落架设计方法的基础上,从工程应用角度出发,总结并提出一套现代民用飞机概念设计阶段起落架接地点设计流程及方法。同时,按照设计流程将影响起落架接地点设计的限制因素划分为适航安全、性能、结构、空间布置、运营等影响因素,明晰各限制因素对设计产生的影响。     

A Poisson multi-Bernoulli mixture filter with spawning based on Kullback–Leibler divergence minimization

In the classical form, the Poisson Multi-Bernoulli Mixture (PMBM) filter uses a PMBM density to describe target birth, surviving, and death, which does not model the appearance of spawned targets. Although such a model can handle target birth, surviving, and death well, its performance may degrade when target spawning arises. The reason for this is that the original PMBM filter treats the spawned targets as birth targets, ignoring the surviving targets’ information. In this paper, we propose a Kullback–Leibler Divergence (KLD) minimization based derivation for the PMBM prediction step, including target spawning, in which the spawned targets are modeled using a Poisson Point Process (PPP). Furthermore, to improve the computational efficiency, three approximations are used to implement the proposed algorithm, such as the Variational Multi-Bernoulli (VMB) filter, the Measurement-Oriented marginal MeMBer/Poisson (MOMB/P) filter, and the Track-Oriented marginal MeMBer/Poisson (TOMB/P) filter. Finally, simulation results demonstrate the validity of the proposed filter by using the spawning model in these three approximations.     

633nm激光波长标准装置

介绍了几种常见的激光稳频技术,分析了基于饱和蒸汽压的碘稳定633nm He-Ne激光系统。激光器的腔长为260 mm,输出功率为0.8 mW,激光调谐范围能够覆盖从a到n的14个吸收峰。通过实验,其频率的相对标准不确定度优于2.5×10-11,1 000 s的频率稳定度优于6×10-12。     

Determination of the threshold value of F10.7 in the dependence of foF2 on solar activity

By introducing the two-segmented linear regression model instead of the well known quadratic fit, we were able to describe the solar activity dependence of the F2 critical frequency. Saturation features were observed and the corresponding F10.7 values at which this phenomenon occurs were obtained for different hours. The seasonal average values were found to be around 154 sfu, 138 sfu, 177 sfu and 150 sfu for March equinox, June solstice, September equinox and December solstice respectively. These affirmed that saturation phenomenon is more pronounced at the equinoxes than solstices. On the average, the threshold value of F10.7 was obtained to be 154.5 sfu for this station in the African sector of the equatorial region.     

Vector quantization for saturated SAR raw data compression

Spaceborne SAR involves the storage and transmission of large-size sampling data. Block adaptive quantization (BAQ) is now the most widely used onboard data compression algorithm due to its good tradeoff between system performance and complexity. However, when spaceborne SAR raw data is saturated, the performance of conventional BAQ deteriorates dramatically because its precondition of Gaussian distribution of raw data no longer holds. In order to solve this problem, an improved vector quantization (VQ) algorithm is proposed. This algorithm firstly introduces saturation modification to a conventional vector quantizer, obtains the saturation codebook based on Gaussian density function, and then obtains the new vector quantizer for the whole set of Saturation Degree (SD). This algorithm makes the vector quantizer match statistical model of data for the whole set of SD, so the performance of the compression is improved. The case of the 2D signal is explicitly computed. The performance of the proposed algorithm is verified by simulated and real data experiments.     

一个湍流谱的进一步研究

一枚Chaff火箭在87.4km高度测量到高达0.33s-1的风切变剖面,相信这个切变值是中层大气曾经测量到的最大切变值.在这个异常大风切变层内,垂直速度扰动谱在浮力子区,惯性子区,和粘性子区有谱斜率-3.10,-1.65,和-7.11,这个观测与中性密度扰动一致.计算的内尺度和浮力尺度与扰动谱中的崩溃点不一致,这个结果与中性密度扰动不一致.讨论了湍流和重力波之间的关系,结果表明,增强湍流与波场饱和有好的联系.      

卫星姿控发动机高空羽流场工程分析

发展卫星姿控小推力发动机高空羽流场的工程估算方法,计算分析其主要燃气组分的分布特征.采用网格技术将发动机喷管出口截面剖分形成多独立点源,建立了非均匀出口流动条件下的分析模型.与自由分子单一点源模型相比,该模型的计算结果更接近实验值.对MBB 10 N双组元发动机多组分羽流场的研究表明,压强场和内能场的变化较剧烈;不同于轻分子组分,重分子组分主要集中于轴线附近,其密度场呈较强方向性.