航天器软件参数修改的测试策略研究

梳理了现有的回归测试策略,并结合航天器软件参数修改错误的2个实例分析,提出了一种新的回归测试策略。该策略借鉴回归测试用例集约简算法中的需求驱动方法,提出了基于构建程序-需求覆盖矩阵和测试用例-需求覆盖矩阵进行回归测试的方法,并给出了按照该策略实施软件参数修改测试的流程。最后,提出了将该测试策略工具化的设想,如研发代码变更影响域自动分析工具,或者使用已有的商用工具。     

TC4板材组织特征与超声检测信号对应关系研究

在大厚度板材在轧制过程中,由于工艺控制不当易引起材料组织分布不均匀、粗大晶粒等问题,本文针对TC4轧制板材研究超声检测信号对材料内部组织分布的表征情况。结果表明,声波垂直于板材流线方向入射时,声衰减分布均匀;而平行入射时,声衰减分布极不均匀,呈条带状分布。为此,对引起不同声波衰减的截面进行组织分析,金相观察发现超声波衰减与材料内部α相的分布及形态有关：声衰减小的区域,材料内部等轴α相较多,晶粒细小,分布均匀;声衰减大的区域,α相被明显拉长。     

Surface strengthening and grain refinement of AZ31B magnesium alloy by ultrasonic cavitation modification

Ultrasonic cavitation modification (UCM) employs cavitation effect to induce strong plastic deformation on the material surface and improve surface properties. To explore the surface strengthening and grain refinement of materials by UCM, the UCM orthogonal experiments of AZ31B magnesium alloy were carried out in water and kerosene, respectively. The effects of ultrasonic amplitude, distance from the sample, and processing time on Vickers hardness and grain size of the material were studied. The results showed that the Vickers hardness of samples increased to 1.5–3 times after UCM in water, which was 23.77–48.19% higher than that in kerosene. The metallographic observation indicated the grains on the surface of AZ31B were refined after UCM. The maximum fluctuation of grain size on the material surface was not more than 10 μm after UCM in water, and most of them were concentrated between 1.5 μm and 2.5 μm, while the former was more than 40 μm and the latter were concentrated between 2 μm and 10 μm in kerosene. This reflected that the grain refinement effect of UCM in water was better than that in kerosene. Ultrasonic cavitation can be used as a benign means to improve the surface properties of materials.     

基于模糊理论的复合材料超声检测缺陷类型识别

本文以复合材料常见缺陷分层、孔隙、疏松的超声波检测缺陷信号为研究对象,选取缺陷波的时域及频域特征,考虑到各特征量之间的不可避免地存在耦合关系,而且对缺陷区分的重要性、敏感度也有很大的差别,采用加权多面体隶属度概念构造隶属函数,依据最大隶属原则进行模式识别,从而区分复合材料缺陷类型。     

基于P～t曲线的导弹火工品品质测试

为了提高导弹火工品的存贮安全性和使用可靠性 ,提出了一种基于P～t(压力 -时间 )曲线获取的火工品品质测试分析方案 ;利用凌华高性能数据采集卡PCI- 9112采集爆炸过程的瞬态压力信号 ,并在对采集到的信号进行频谱分析和在滤波的基础上提取出了火工品的特征参数 ,从而为火工品的品质评判提供了决策参考。     

有限元仿真模拟在超声喷水无损检测用水套设计中的应用

水套在超声喷水穿透检测中具有重要作用,为设计出具有良好耦合效果的水套,减少水流紊流对声波耦合的影响,本文通过构建探头套几何模型、物理建模、数值求解的有限元仿真方法对探头水套进行流体动力学仿真。结果表明,在无整流装置下,从入水口射入的水流撞击探头套内壁,产生严重紊流,进入出水管后,紊流状态仍然保持,水流流线方向杂乱。增加整流装置后,探头套内紊流得到很好的抑制,使得进入出水管的水流流线方向趋向一致,这种现象随着整流片增多而效果越加明显。本文为后续模拟水流经过出水口后的水柱状态,特别是随着初始水流速度加大后的水柱状态,以及利用有限元多物理场模拟功能,在加入声场后,模拟紊流状况下声场的变化打下了基础。     

虚拟仪器的超声检测系统在航空维修中的应用

为实现对海军琶机结构损伤的检测智能化,应用超声检测和虚拟仪器技术,研制了基于虚拟仪器的超声检测系统。应用该系统对某型进口直升机尾桨叶和某型运输机的螺栓进行了检测,结果表明仪器达到了设计要求,满足了航空维修无损检测需要。     

固体火箭发动机封头界面粘接相控阵超声检测技术可行性研究

固体火箭发动机封头部分的界面粘接状态目前还没有有效的检测方法,采用相控阵超声自动电子聚焦技术为该结构的检测提供了新思路.根据声线理论,研究等厚、不等厚壳体的界面粘接相控聚焦检测方式,得出相控聚焦具有较高的检测分辨率,同时也能解决不等厚壳体构件的界面粘接检测;对固体火箭发动机封头构件的粘接状态进行仿真分析,结果显示相控阵超声能很好地检测出构件的脱粘区域和大小,表明该检测方式在界面粘接检测方面具有广泛的应用前景.     

不同透气情况降落伞的流场试验研究

降落伞由于其柔软透气性,其流场测量非常困难,而流场特性直接关系到降落伞的气动性能.本文采用风洞设备,利用七孔探针对不同透气情况下的降落伞的绕流流场进行了试验测量.采用Labview和Matlab engine混合编程技术进行七孔探针的压力数据采集和实时数据处理,获得了不同透气情况下伞衣周围的速度及压力分布情况,并对其进行了详细的流场分析.通过对不同透气伞流场的比较,可知透气情况对伞衣前后静压大小、尾流流线汇集位置、稳定性及噪音均有一定的影响.本文的研究解决了绕伞衣流场定量测量的难题,同时为降落伞的气动性能分析提供了一个很好的技术方案.     

Grouping bi-chi-squared method for pulsar navigation experiment using observations of Rossi X-ray timing explorer

X-ray pulsar-based navigation is a revolutionary technology which is capable of providing the required navigation information in the solar system. Performing as an important pulsar-based navigation technique, the Significance Enhancement of Pulse-profile with Orbit-dynamics (SEPO) can estimate orbital elements by using the distortion of pulse profile. Based on the SEPO technique, we propose a grouping bi-chi-squared technique and adopt the observations of Rossi X-ray Timing Explorer (RXTE) to carry out experimental verification. The pulsar timing is refined to determine spin parameters of the Crab pulsar (PSR B0531+21) during the observation periods, and a short-term dynamic model for RXTE satellite is established by considering the effects of diverse perturbations. Experimental results suggest that the position and velocity errors are 16.3 km (3σ) and 13.3 m/s (3σ) with two adjacent observations split by one day (exposure time of 1.5 ks), outperforming those of the POLAR experiment whose results are 19.2 km (3σ) and 432 m/s (3σ). The approach provided is particularly applicable to the estimation of orbital elements via using high-flux observations.